|
A Two-Phase Investigation of Longitudinal Flying Qualities for Fighters
Report Number: AFFDL TR 74-9
Author(s): Edward M. Boothe; Robert T. N. Chen; Charles R. Chalk
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1974
Pages: 292
Contract: F33615-73-C-3051
Project: None Given
Task: None Given
AD Number: AD0782218
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails:  (292 pages, 6.942 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 Flight Investigation and Analysis of Longitudinal Handling Qualities of STOL Aircraft on Landing Approach
Report Number: AFFDL TR 74-18
Author(s): K-H. Doetsch, Jr.; D. W. Laurie-Lean
Corporate Author: National Research Council of Canada
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1974
Pages: 318
Contract: F33615-71-C-1722
Project: None Given
Task: None Given
AD Number: ADA001596
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (318 pages, 7.727 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
Leeside Flow Field Description Over Cones at Large Incidence
Report Number: AFFDL TR 74-19
Author(s): Victor Zakkay; Constatino Economos; Edgar Alzner
Corporate Author: Advanced Technology Laboratories, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1974
Pages: 88
Contract: F33615-73-C-3010
Project: None Given
Task: None Given
AD Number: AD0785369
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (88 pages, 1.531 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 Response of Aircraft Encountering Aircraft Wake Turbulence
Report Number: AFFDL TR 74-29
Author(s): Robert C. Nelson
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1974
Pages: 142
Contract: Laboratory Research - No Contract
Project: None Given
Task: None Given
AD Number: AD0787193
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (142 pages, 1.677 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 Approximate Solution of Unsteady Transonic Flow Problems
Report Number: AFFDL TR 74-32
Author(s): K. R. Kimble; J. M. Wu
Corporate Author: University of Tennessee Space Institute
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1974
Pages: 40
Contract: F33615-73-C-3119
Project: 1929
Task: 192905
AD Number: AD0783621
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (40 pages, 0.611 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 Numerical Solution of the Asymptotic Equations of Trailing Edge Flow
Report Number: AFFDL TR 74-46
Author(s): Charles E. Jobe
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 10/1/1974
Pages: 114
Contract: Laboratory Research - No Contract
Project: 1476
Task: 147601
AD Number: ADA003668
Photo Enhancement: Not Needed
Notes: Due to printing problem, p20-21 & 80-81 are blank
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (114 pages, 1.83 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
Program Summary for Control Configured Vehicle Concepts Applied to Fighter Aircraft
Report Number: AFFDL TR 74-51
Author(s): Dwight Bennet, et al
Corporate Author: McDonnel Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1974
Pages: 191
Features: + Foldout(s)
Contract: F33615-72-C-1286
Project: 487T
Task: None Given
AD Number: ADB002700
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is considered Limited Distribution by DoD and Contrails staff cannot supply 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
Final Report on Program to Improve MIL-F-83300
Report Number: AFFDL TR 74-54
Author(s): Charles R. Chalk; Robert C. Radford; Richard Wasserman
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1974
Pages: 168
Contract: F33615-71-C-1722
Project: None Given
Task: None Given
AD Number: ADA001598
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (168 pages, 3.546 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 Analytic and Experimental Investigation of the Wakes Behind Flapped and Unflapped Wings
Report Number: AFFDL TR 74-90
Author(s): Alan J. Bilanin; Coleman duP. Donaldson; Richard S. Snedeker
Corporate Author: Aeronautical Research Associates of Princeton, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1974
Pages: 142
Contract: F33615-73-C-3138
Project: None Given
Task: None Given
AD Number: ADA021344
Photo Enhancement: Complete
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (142 pages, 2.661 MB)
Via DTIC Online:
This report is available for download via DTIC Online: (140 pages, 5 MB)
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
Review of Methods of Solution of Afterbody/Exhaust Nozzle Flow Fields
Report Number: AFFDL TR 74-108
Author(s): Wladimiro Calarese
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1974
Pages: 164
Contract: Laboratory Research - No Contract
Project: 1476
Task: None Given
AD Number: AD0787459
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (164 pages, 2.464 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
Sonic Fatigue Design Guide for Military Aircraft
Report Number: AFFDL TR 74-112
Author(s): F. F. Rudder Jr.; H. E. Plublee Jr.
Corporate Author: Acoustic & Vibration Associates
Corp. Rep. Number: AVA/TR 73-280
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1975
Pages: 600
Contract: F33615-73-C-3124
Project: 1471
Task: 147101
AD Number: ADB004600
Abstract Text:
Accurate methods are presented for estimating the acoustic loading, structural response, and fatigue life of military aircraft structures. This report presents over sixty tables, 110 charts and nomographs, five computer programs and forty worked examples illustrating the use of the different methods. These results stem from a review and evaluation of over 300 references related to the various topics associated with sonic fatigue. This report is organized into independent sections with the subject classification allowing for ease of identification and future extension as required. Sufficient detail is provided so that the entire handbook stands as an independent source of sonic fatigue design data.
Options for obtaining report:
Via Contrails:
Contrails does not possess this report.
Via DTIC Online:
This report is available for download via DTIC Online: (600 pages, 17 MB)
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
Background Information and User Guide for MIL-F-9490D
Report Number: AFFDL TR 74-116
Author(s): James L. Townsend; Eugene T. Raymond
Corporate Author: Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 1/1/1975
Pages: 248
Contract: F33615-72-C-1090
Project: 8225
AD Number: ADA029074
Photo Enhancement: Not Needed
Abstract Text:
This document is published in support of Military Specification MIL- F-9490D, 'Flight Control Systems - Design, Installation and Test of, Piloted Aircraft, General Specification For'. It was written to aid the MIL-F-9490D user in interpretation and use of the specification. The philosophy adopted by the Air Force for this revision of MIL-F-9490 is discussed and, where pertinent, the limitations of the data or arguments used to support individual requirements are stated. Pertinent literature has also been referenced in conjunction with individual requirements, where recent supporting research and development has been accomplished.
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (248 pages, 8.381 MB)
Via DTIC Online:
This report is available for download via DTIC Online: (251 pages, 13 MB)
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 and Simulation of Variable Throttle/Energy Management Concepts for Fighter Aircraft
Report Number: AFFDL TR 74-138
Author(s): G. G. Grose; R. J. Landy; R. G. Marsh; R. D. Turner
Corporate Author: McDonnell Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 11/1/1974
Pages: 153
Contract: F33615-73-C-3130
Project: 1987
Task: 198702
AD Number: ADA006745
Photo Enhancement: Not Needed
Options for obtaining report:
Via Contrails:
This report is avalable for download via Contrails: (153 pages, 3.359 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
|
