|
Aerodynamic Stability and Control/Wind Tunnel Data Correlation
Report Number: AFFDL TR 71-3
Author(s): G. R. Casteel
Corporate Author: North American Rockwell Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1971
Pages: 220
Contract: AF 33(615)-5323
AD Number: AD0726103
Photo Enhancement: Complete
Abstract Text:
The general objective was to collect and analyze aerodynamic stability and control data for the XV-4B, XV-5A, and P-1127 VTOL configurations. Correlation and analysis of existing model data were made to investigate hover and transition characteristics. Particular emphasis was placed on the aerodynamic power effects, sometimes referred to as interference effects. Other areas of investigation were sometimes referred to as interference effects. Other areas of investigation were nondimensional coefficients used to present VTOL data and wind tunnel test techniques. Wind tunnel tests were conducted using an inlet only model and a jet only model to investigate special test and analysis problems for these components. The agreement between different sets of XV-4B model data was, in general, found to be poor. However, the nondimensional coefficients used by Lockheed to reduce to XV-4B model data appear to be valid parameters for this category of VTOL airplane. The jet entrainment flow was shown by experiment to be the primary cause of the XV-4B power effects, and the XV-4B jet path was experimentally and theoretically determined.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails:  (220 pages, 5.074 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Air-Cushion Pressure During Stiff-Operation for Air-Cushion Landing Systems. Part II. Experiments.
Report Number: AFFDL TR 71-4 Part 2
Author(s): Han, Lit S.
Corporate Author: Ohio State Univ Research Foundation Columbus
Publication Date: 3/1/1972
Pages: 104
Project: 0
Task: 0
AD Number: AD0750936
Photo Enhancement: Complete
Abstract Text:
The report describes the experimental verification of the theory developed in Part I for ACLS in its stiff-mode operation. It also reports the discharge coefficient data required for computing air flow requirements. At low ground clearances, the theory was verified to be in excellent agreement with the experimental data obtained. At higher values of the ground clearance where the viscous flow theory is not expected to hold, appreciable difference between the experimental data and theoretical computation was observed. A multi-jet theory yet to be developed is expected to bridge the gap.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (104 pages, 17.318 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Study of Folding Proprotor VTOL Aircraft Dynamics. Volume I. Analytical Methods.
Report Number: AFFDL TR 71-7 Volume 1
Author(s): Yen, Jing G.; Weber, Gottfried E.; Gaffey, Troy M.
Corporate Author: Bell Helicpter Textron Inc., Fort Worth, Texas
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1971
Pages: 282
Features: + Foldout(s)
Contract: F33615-69-C-1339
Project: 1370
Task: 137005
AD Number: AD0889039
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (282 pages, 15.819 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Collapse Analysis for Shells of General Shape; Volume I. Analysis.
Report Number: AFFDL TR 71-8 Volume 1
Author(s): Almroth, B. O.; Brogan, F. A.; Marlowe, M. B.
Corporate Author: Lockheed Missiles And Space Co Palo Alto Calif Palo Alto Research Lab
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1972
Pages: 90
Contract: F33615-69-C-1523
Project: None Given
Task: None Given
AD Number: AD0751702
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (90 pages, 1.332 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Survivable Flight Control System Interim Report No. 1: Studies, Analyses and Approach
Report Number: AFFDL TR 71-20
Author(s): David S. Hooker; Rober I. Kisslinger; George R. Smith; M. Sheppard Smyth
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1971
Pages: 375
Features: + Foldout(s)
Contract: F33615-69-C-1827
Project: 680J
Task: None Given
AD Number: AD0733582
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (375 pages, 25.519 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Survivable Flight Control System Interim Report No. 1 Studies, Analyses and Approach: Supplement for Control Criteria Studies
Report Number: AFFDL TR 71-20 Supplement 1
Author(s): Robert L. Kisslinger; Michael J. Wendl
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1971
Pages: 198
Contract: F33615-69-C-1827
Project: None Given
Task: None Given
AD Number: AD0727762
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (198 pages, 4.638 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Survivable Flight Control System Interim Report No. 1 Studies, Analyses, and Approach: Supplement for Control Law Development Studies
Report Number: AFFDL TR 71-20 Supplement 2
Author(s): Robert L. Kisslinger; George J. Vetsch
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboartory
Publication Date: 5/1/1971
Pages: 354
Features: + Foldout(s)
Contract: F33615-69-C-1827
Project: None Given
Task: None Given
AD Number: AD0729207
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (354 pages, 54.719 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Survivable Flight Control System Interim Report No. 1 Studies, Analyses and Approach: Supplement for Hydraulic Power and Actuation Studies
Report Number: AFFDL TR 71-20 Supplement 3
Author(s): Gerald E. Amies; Cecil Clark; Charles L. Jones; M. Sheppard Smith
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1971
Pages: 253
Features: + Foldout(s)
Contract: F33615-69-C-1827
Project: None Given
Task: None Given
AD Number: AD0727763
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (253 pages, 13.271 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
The Generation of a Military Specification for Flying Qualities of Piloted V/STOL Aircraft - MIKL-F-83300
Report Number: AFFDL TR 71-23
Author(s): David L. Key
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1971
Pages: 42
Contract: AF 33(615)-3736
Project: 698DC
Task: None Given
AD Number: AD0725746
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (42 pages, 1.169 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Statistical Analysis of LO-LOCAT Turbulence Data for Use in the Development of Revised Gust Criteria
Report Number: AFFDL TR 71-29
Author(s): McCloskey, John W.; Luers, James K,; Ryan, John P.; Engler, Nicholas A.
Corporate Author: Dayton University Research Institute
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1971
Pages: 140
Contract: F33615-69-C-1477
Project: None Given
Task: None Given
AD Number: AD0731139
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (140 pages, 3.518 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Theory of an Air Cushion Landing System for Aircraft
Report Number: AFFDL TR 71-50
Author(s): Digges, Kennerly H.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1971
Pages: 324
Contract: Laboratory Reseach - No Contract
Project: 1369
Task: 136907
AD Number: AD0728647
Photo Enhancement: Complete
Abstract Text:
The Air Cushion Landing System is a scheme to replace the wheeled landing gear on aircraft by a peripheral jet air cushion. The concept employs a flexible elastic membrane or 'trunk' which is attached to the bottom of the aircraft fuselage. During flight, the trunk shrinks elastically and hugs the bottom of the fuselage like a de-icing boot. When a flow of air is applied to the inside of the trunk, the elastic material stretches and forms an elongated doughnut-shaped protrusion on the underside of the aircraft. The air flow is ducted by the trunk to the fuselage periphery and exhausted through a large number of holes or slots. As a result, a pressure builds up under the aircraft when the ground is approached. The pressure is sufficient to support the aircraft and absorb its vertical landing velocity. The study develops analytical relationships between the variables associated with the Air Cushion Landing System. Included are the following: The derivation of a theory which predicts the static characteristics of the system; Analytical methods for predicting flow, jet height and power requirements; Curves which illustrate the interrelationships among the design variables; Computer programs for predicting the cross-sectional area and shape of the elastic trunk; The development and test of an analytical model which predicts the dynamic response of the system to landing impact; A discussion of the design considerations for the system.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (324 pages, 23.176 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume I. Parametric Design Studies.
Report Number: AFFDL TR 71-62 Volume 1
Author(s): Fry, Bernard L.
Corporate Author: Boeing Vertol Company, Philadelphia, Pennsylvania
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1971
Pages: 326
Features: + Foldout(s)
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0729427
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (326 pages, 6.693 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume II. Component Design Studies.
Report Number: AFFDL TR 71-62 Volume 2
Author(s): Fry, Bernard L.
Corporate Author: Boeing Vertol Company, Philadelphia, Pennsylvania
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1971
Pages: 151
Features: + Foldout(s)
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0729428
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (151 pages, 3.323 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume III - Appendixes
Report Number: AFFDL TR 71-62 Volume 3
Author(s): Bernard L. Fry
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1971
Pages: 150
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0729429
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (150 pages, 2.474 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Volume IV. Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part I. Analysis and Results
Report Number: AFFDL TR 71-62 Volume 4 Part 1
Author(s): John Magee; Robert Taylor
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1971
Pages: 140
Contract: F33615-69-C-1577
Project: 69BT
Task: None Given
AD Number: AD0735632
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (140 pages, 2.809 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Volume IV. Wind Tunnel Test of the Concersion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model: Part II. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details
Report Number: AFFDL TR 71-62 Volume 4 Part 2
Author(s): John Magee; Robert Taylor
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1971
Pages: 83
Contract: F33615-69-C-1577
Project: 69BT
Task: None Given
AD Number: AD0735733
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (83 pages, 1.925 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Volume V. Wind Tunnel Test of a Powered Tilt-Rotor Perfromance Model
Report Number: AFFDL TR 71-62 Volume 5
Author(s): John P. Magee; Robert B. Taylor; Frank J. McHugh; Nelson Miller; Leon N. DeLarm
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 508
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0736824
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (508 pages, 10.94 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Volume VI. Wind Tunnel Test of a Powered Tilt-Rotor Dynamic Model on a Simulated Free Flight Suspension System
Report Number: AFFDL TR 71-62 Volume 6
Author(s): John E. Tomassoni; Robert B. Taylor; Leon N. Delarm; Edward B. Schagrin
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 208
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0735633
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (208 pages, 4.82 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Volume VII. Wind Tunnel est of the Aerodynamics and Dynamics of Rotor Spinup, Stopping and Folding on a Semispan Folding Tilt-Rotor Model
Report Number: AFFDL TR 71-62 Volume 7
Author(s): Dirk van Wagensveld; Frank J. McHugh; Leon N. Delarm; Walter L. Lapinski;m John P. Magee
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 400
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0736825
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (400 pages, 8.148 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume VIII. Summary of Structural Design Criteria and Aerodynamic Prediction Techniques
Report Number: AFFDL TR 71-62 Volume 8
Author(s): Robin W. Sandford; Francis J. McHugh; Leon N. Delarm; Edward B Schasgrin; John P. Magee
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 280
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0736021
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (280 pages, 6.293 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Design Studies and Model Tests of the Stowed Tilt Rotor Concept: Volume IX. Value Engineering Report
Report Number: AFFDL TR 71-62 Volume 9
Author(s): Jaan Liiva; H. J. Rose
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 63
Features: + Foldout(s)
Contract: F33615-69-C-1577
Project: None Given
Task: None Given
AD Number: AD0736022
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (63 pages, 2.595 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Preliminary Handling Qualities Requirements for Lifting Re-Entry Vehicles During Terminal Flight
Report Number: AFFDL TR 71-64
Author(s): Dante A. Di Franco; John F. Mitchell
Corporate Author: Corenell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboartory
Publication Date: 8/1/1971
Pages: 246
Contract: F33615-70-C-1755
Project: 680A
Task: None Given
AD Number: AD0731563
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (246 pages, 7.616 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Analysis of Structural Shells with Transverse Shear Deformation
Report Number: AFFDL TR 71-116
Author(s): Richard L. Citerley
Corporate Author: Anamet Laboratories, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1971
Pages: 200
Contract: AF 33(615)-70-1019
Project: None Given
Task: None Given
AD Number: AD0736052
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (200 pages, 5.031 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Total In-Flight Simulator (TIFS) - Preliminary Design Report
Report Number: AFFDL TR 71-119
Author(s): None Given
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1971
Pages: 264
Contract: F33615-67-C-1157
Project: 684B
Task: None Given
AD Number: AD0738314
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (264 pages, 5.754 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Development of Weapon Delivery Models and Analysis Programs. Volume I. System Modeling and Performance Optimization.
Report Number: AFFDL TR 71-123 Volume 1
Author(s): Konar, A. Ferit
Corporate Author: Honeywell Inc Minneapolis Minn Systems And Research Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1972
Pages: 210
Contract: F33615-71-C-1059
Project: 8219
Task: 821911
AD Number: AD0751505
Photo Enhancement: Not Needed
Abstract Text:
The concern in the work reported is the development of a dynamic precision weapon delivery system model for analyzing the effects of system parameters and disturbances on delivery performance. In addition, a methodology of precision weapon delivery flight control design is developed, without considering the pilot as a control element. The aircraft model accommodates a wide variety of airframe nonlinear dynamics, control points and methods and measurement systems. The bomb model is general enough for a variety of dive-bomb angles, release altitudes and release speeds. The circular error probable (CEP) at impact is chosen as a measure of weapon delivery performance, and a technique is developed for relating the effects of flight control parameters, airframe dynamics, measurement errors and gust disturbances to this measure by using the system model. Demonstration analysis is performed to show how to identify critical system parameters with regard to the delivery of an iron bomb and to illustrate how the method of analysis can be used. Digital computer subprograms (in FORTRAN 4 language) were developed and documented implementing the mathematical models.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (210 pages, 6.511 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Development of Weapon Delivery Models and Analysis Programs. Volume II. Documentation of the Armament Delivery Analysis Programming System (ADAPS).
Report Number: AFFDL TR 71-123 Volume 2
Author(s): Konar, A. Ferit; Ward,Michael D.
Corporate Author: Honeywell Inc Minneapolis Minn Systems And Research Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1972
Pages: 316
Contract: F33615-71-C-1059
Project: 8219
Task: 821904
AD Number: AD0751506
Photo Enhancement: Not Needed
Abstract Text:
Development of Weapon Delivery Models and Analysis Programs. Volume II. Documentation of the Armament Delivery Analysis Programming System (ADAPS).Final technical rept. 5 Oct 70-5 Oct 71,FKonar,A. Ferit ;Ward,Michael D. ;12261-FR1-Vol-2F33615-71-C-1059AF-8219821904AFFDLTR-71-123-Vol-2See also Volume 1, AD-751 505.(*close support, mathematical models), (*bomb trajectories, circular error probable), (*aircraft guns, effectiveness), computer programs, rockets, flight control systems, gust loads, miss distance, weapon systems, equations of motion, partial differential equations, perturbation theory, white noise, numerical analysisadap computer program, automatic, control, bomb release point, fortran, fortran 4 programming language, control theoryThe computer programs which implement the mathematical analysis and models developed in Volume I (AD-751 505) are described. The programs are developed in FORTRAN 4 language. Extensive use of subroutines is made to provide programming flexibility when considering alternate airframe/dynamics/control points/ measurement system combinations and their effect on weapon-delivery performance.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (316 pages, 9.133 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Development of Weapon Delivery Models and Analysis Programs. Volume III. Testing and Demonstration of the Armament Delivery Analysis Programming System (ADAPS).
Report Number: AFFDL TR 71-123 Volume 3
Author(s): Konar, A. Ferit; Ward, Michael D.
Corporate Author: Honeywell Inc Minneapolis Minn Systems And Research Div
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1972
Pages: 194
Contract: F33615-71-C-1059
Project: 8219
Task: 821904
AD Number: AD0751527
Photo Enhancement: Not Needed
Abstract Text:
The testing and use of ADAPS is demonstrated by performing an analysis with a specified iron bomb (M117) and a representative tactical fighter-bomber aircraft (F4). The demonstration example revealed no appreciable performance difference between the time-invariant and time-invariant and time-varying optimal controllers for the weapon delivery process. The contribution matrix of an iron bomb indicated that the major contributors to the CEP are the velocity and the attitude-state errors at release.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (194 pages, 4.808 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Fabrication and Instrumentation of an Experimental Passive Radiative Infrared Detector Cooler for Spacecraft Applications
Report Number: AFFDL TR 71-125
Author(s): W. F. Schmidt; H. L. Hillesland; C. A. Zierman
Corporate Author: Philco-Ford Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 78
Contract: F33615-71-C-1025
Project: None Given
Task: None Given
AD Number: AD0893616
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (78 pages, 2.326 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Validation of the Flying Qualities Requirements of MIL-F-8785B (ASG)
Report Number: AFFDL TR 71-134
Author(s): R. N. Kandalft
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1971
Pages: 440
Contract: F33615-71-C-1065
Project: 8219
Task: 821905
AD Number: AD0738625
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (440 pages, 11.994 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
In-Flight Test Results on Mission-Oriented Cockpit Lighting Requirements
Report Number: AFFDL TR 71-142
Author(s): C. J. DeBruine; J. R.Milligan
Corporate Author: Lear Siegler, Inc.; North American Rockwell Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1971
Pages: 140
Contract: F33615-69-C-1709
Project: 6190
Task: None Given
AD Number: AD0749478
Photo Enhancement: Incomplete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (140 pages, 3.751 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Preliminary Design Study for an Advanced Fighter Type In-Flight Simulator
Report Number: AFFDL TR 71-149
Author(s): J. T. Gallagher; I. Saworotnow; R. J. Seemann
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1971
Pages: 277
Features: + Foldout(s)
Contract: F33615-71-C-1366
Project: 8219
Task: 821905
AD Number: AD0743970
Photo Enhancement: Incomplete
Options for obtaining report:
Via Contrails:
This report has yet to be scanned by Contrails staff.
Click here to request scanning of this report
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Investigation of Measuring System Requirements for Low Visibility Landing
Report Number: AFFDL TR 71-151
Author(s): Lee Gregor Hofmann; Warren F. Clement; Dunstan Graham; Richard E. Blodgett; Kishor V. Shah
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1971
Pages: 162
Contract: F33615-70-C-1621
Project: 404L
Task: 404L0101
AD Number: AD0739932
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (162 pages, 3.384 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Flight Control Principles for Control Configured Vehicles
Report Number: AFFDL TR 71-154
Author(s): Edmund G. Ryanski; Norman C. Weingarten
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 100
Contract: F33615-71-C-1238
Project: 8226
AD Number: AD0749479
Photo Enhancement: Not Needed
Abstract Text:
The compatibility between maneuver load control, relaxed static stability, and flying qualities requirements is investigated in the report. Three steps were involved in the investigation: an analysis was made of control surface combinations and their effectiveness for maneuver load control when used with an airplane having shortened tail length and reduced tail surface area, control system configurations were synthesized that minimize a weighted measure of change in drag, wing root bending moment, control surface activity and response error between a Level 1 flying qualities model and the actual T-33 airplane; and a direct optimization of the tail length, tail area and control surface deflections required to obtain a compatible compromise of the CCV objectives was performed.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (100 pages, 2.052 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Takeoff and Landing Analysis (TOLA) Computer Program: Part I. Capabilities of the Takeoff and Landing Analysis Computer Program
Report Number: AFFDL TR 71-155 Part 1
Author(s): Urban H. D. Lynch
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 50
Contract: Laboratory Research - No Contract
Project: 1431
Task: 143109
AD Number: AD0741942
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (50 pages, 0.714 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Study of the Practicability of Active Vibration Isolation Applied to Aircraft during the Taxi Condition.
Report Number: AFFDL TR 71-159
Author(s): Corsetti, Charles D.; Dillow, James D.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB Ohio
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1972
Pages: 170
Contract: Laboratory Research - No Contract
Project: 8219
Task: 821904
AD Number: AD0750137
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (170 pages, 2.296 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Prediction and Evaluation of Flying Qualities in Turbulence
Report Number: AFFDL TR 71-162
Author(s): E. D. Onstott; E. P. Salmon; R. L. MCCormick
Corporate Author: Northrop Corporation Aircraft Division
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 392
Contract: F33615-71-C-1076
Project: 8219
Task: 821904
AD Number: AD0749480
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (392 pages, 4.411 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
In-Flight Investigation of an Unaugmented Class III Airplane in the Landing Approach Task Phase I - Lateral Directional Study
Report Number: AFFDL TR 71-164 Volume 1
Author(s): Richard Wasserman; Franklin F. Eckhart; Howard J. Ledder
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 272
Contract: F33615-71-C-1110
Project: None Given
Task: None Given
AD Number: AD0744831
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (272 pages, 6.841 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Method for the Prediction of Performance of STOL High Lift Systems Near Maximum Lift Coefficient
Report Number: AFFDL TR 71-169
Author(s): Paul T. Bauer
Corporate Author: University of Dayton Research Institute
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1971
Pages: 54
Contract: F33615-70-C-1019
Project: None Given
Task: None Given
AD Number: AD0740476
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (54 pages, 1.183 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Variable Diameter Rotor Study
Report Number: AFFDL TR 71-170
Author(s): Arthur W. Linden, et al
Corporate Author: Sikorsky Aircraft
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1972
Pages: 198
Features: + Foldout(s)
Contract: F33615-71-C-1186
Project: 1366
Task: 136617
AD Number: AD0740911
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (198 pages, 11.33 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Take-Off and Landing Critical Atmospheric Turbulence (TOLCAT) Experiments and Analysis
Report Number: AFFDL TR 71-172
Author(s): C. E. Elderkin; D. C. Powell; A. G. Dunbar; T. W. Horst
Corporate Author: Battelle Memorial Institute
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1972
Pages: 306
Contract: F33516-68-M-5009
Project: None Given
Task: None Given
AD Number: AD0750131
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (306 pages, 7.575 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
An Assessment of the "Paper Pilot" - An Analytical Approach to the Specification and Evaluation of Flying Qualities
Report Number: AFFDL TR 71-174
Author(s): Gary L. Teper
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 116
Features: + Foldout(s)
Contract: F33615-71-C-1071
Project: 8219
Task: None Given
AD Number: AD0755367
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report has yet to be scanned by Contrails staff.
Click here to request scanning of this report
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Analysis of Data Rate Requirements for Low Visibility Approach with a Scanning Beam Landing Guidance System
Report Number: AFFDL TR 71-177
Author(s): James D. Dillow; Paul R. Stolz; Meyer D. Zuckerman
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1973
Pages: 176
Contract: Laboratory Research - No Contract
Project: 8219
Task: 821911
AD Number: AD0758786
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (176 pages, 2.901 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Implementation Studies for a Reliability-Based Static Strength Criteria System: Volume I, Evaluation
Report Number: AFFDL TR 71-178 Volume 1
Author(s): M. C. Campion, L. C. Hanson; D. S. Morcock, et al.
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 192
Contract: F33615-71-C-1129
Project: 1367
Task: 136714
AD Number: AD0742260
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (192 pages, 2.995 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Implementation Studies for a Reliability-Based Static Strength Criteria System: Volume II, Implementation
Report Number: AFFDL TR 71-178 Volume 2
Author(s): M. C. Campion, W. D. Campbell; J. W. Chapman, et al.
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1972
Pages: 244
Contract: F33615-71-C-1129
Project: 1367
Task: 136714
AD Number: AD0742261
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (244 pages, 4.333 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Prediction methods for Near Field Noise Environments of VTOL Aircraft
Report Number: AFFDL TR 71-180
Author(s): L. C. Sutherland; D. Brown
Corporate Author: Wyle Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1972
Pages: 246
Contract: F33615-69-C-1407
Project: 1471
Task: 147102
AD Number: AD0900405
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (246 pages, 5.327 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
Study of the Blunt Slab Delta Wing at Hypersonic Speeds and Angles of Attack
Report Number: AFFDL TR 71-181
Author(s): Burke, Gerald L.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1972
Pages: 74
Contract: Laboratory Research - No Contract
Project: 1366
Task: 136607
AD Number: AD0902598
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (74 pages, 1.536 MB)
Via DTIC Online:
This report is not available for download via DTIC Online
Via NASA Technical Report Server:
This report is not available for download via NTRS
Via National Technical Information Service:
Indications of Public Availabilty:
No digitial image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement
|
