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Prediction, Evaluation, and Specification of Closed Loop and Multiaxis Flying Qualities
Report Number: AFFDL TR 78-3
Author(s): E. D. Onstott; W. H. Faulkner
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1978
Pages: 286
Contract: F33615-77-C-3008
Project: 2307
Task: 230703
AD Number: ADA056983
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Factor of Safety - USAF Design Practice
Report Number: AFFDL TR 78-8
Author(s): Geogre E. Miller and Clement J. Schmid
Corporate Author: Structural Integrity Branch
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1978
Pages: 104
Contract: Laboratory Research - No Contract
Project: 2401
Task: 240101
AD Number: ADA070237
Photo Enhancement: Complete
Abstract Text:
A review of the historical development of the 1.5 structural factor of safety for airplanes, the 1.4 factor for manned space vehicles, and the 1.25 factor for missiles is presented from an Air Force perspective. Several variations and experimental applications of the factor of safety design concept and reliability based design concepts are also reviewed to show their interaction. Although not without criticism, the factor of safety design concept has become an almost universally accepted measure of flight safety. There is, however, a tendency among engineers to both challenge the continued application of factors of safety for efficient airframe design, and yet to avoid any changes that would challenge the confidence of future designs. The use of reliability based concepts will probably increase but their application to airframe design may be limited. The factor of safety still covers many contingencies and it appears at this time there will be a continuing need for some factor.
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Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes
Report Number: AFFDL TR 78-16
Author(s): Robert M. Kulfan and John D. Vachal
Corporate Author: Boeing Commercial Airplane Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 2/1/1978
Pages: 71
Contract: F33615-76-C-3035
Project: 2404
Task: 240410
AD Number: ADA056124
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Notes: Cover is missing 'Transport' in title
Abstract Text:
A Preliminary Design Study of large turbulent flow military transport aircraft has been made. The study airplanes were designed to carry a heavy payload (350,000 lb) for a long range (10,000 nmi). The study tasks included: Wing geometry/cruise speed optimization of a large cantilever wing military transport airplane; Preliminary design and performance evaluation of a strut-braced wing transport airplane; and Structural analyses of large-span cantilever and strut-braced wings of graphite/epoxy sandwich construction (1985 technology). The best cantilever wing planform for minimum takeoff gross weight, and minimum fuel requirements, as determined using statistical weight evaluations, has a high aspect ratio, low sweep, low thickness/chord ratio, and a cruise Mach number of 0.76. A near optimum wing planform with greater speed capability (M = 0.78) has an aspect ratio = 12, quarter chord sweep = 20 deg, and thickness/chord ratio of 0.14/0.08 (inboard/outboard).
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Analysis of Wind Tunnel Data Pertaining to High Angle-of-attack Aerodynamics Volume II - Database
Report Number: AFFDL TR 78-94 Volume 2
Author(s): J. W. Headley
Corporate Author: Northrup Corporation Aircraft Group
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1978
Pages: 571
Features: + Diagram(s) + Drawing(s) + Graph(s)
Contract: F33615-77-C-3062
Project: 2404
Task: 240410
AD Number: ADA069647
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Abstract Text:
This volume presents, in summary form, the geometric and aerodynamic data used as a basis for the design guidelines presented in Volume I. The summaries have been divided into eight sections, the first seven being the low speed tests, which include almost all the configuration development studies and most of the high AOA testing. Data summaries for the transonic and supersonic testing form the eighth and last section. Because of the considerable quantity of data available from all the testing (some test reports containing as much as thirteen volumes), it is not practical to include the summaries in all the basic aerodynamic data available. In general, only the main aerodynamic effects are presented or summarized, and for more detailed information on a particular configuration, reference should be made to the actual wind tunnel report. All the data summaries are presented in a similar way, and include the following information: a data sheet including the test report title, a summary of the report, and the test conditions; a general three view of a representative test model configuration; detailed sketches of the pertinent configurations changes; and the relevant aerodynamic data.
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Analysis of Digital Flight Control Systems with Flying Qualities Applications: Volume I - Executive Summary
Report Number: AFFDL TR 78-115 Volume 1
Author(s): Richard F. Whitbeck
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1978
Pages: 28
Contract: F33615-77-C-3026
Project: 2307
Task: 230703
AD Number: ADA066809
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Analysis of Digital Flight Control Systems with Flying Qualities Applications: Volume II - Technical Report
Report Number: AFFDL TR 78-115 Volume 2
Author(s): Richard F. Whitbeck; L. G. Hofmann
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1978
Pages: 230
Contract: F33615-77-C-3026
Project: 2307
Task: 230703
AD Number: ADA067177
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Preliminary Design Aerodynamic Prediction Methodology for Missiles with Nose Bluntness
Report Number: AFFDL TR 78-117
Author(s): Charles W. Ingram; Karlheinz O. W. Ball; Carter Dinkeloo; David Shida
Corporate Author: Systems Research Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1978
Pages: 200
Contract: F33615-75-D-0089/0030
Project: None Given
Task: None Given
AD Number: ADA073664
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Effects of Control System Dynamics on Fighter Approach and Landing Longitudinal Flying Qualities: Volume I
Report Number: AFFDL TR 78-122
Author(s): Rogers E. Smith
Corporate Author: Calspan Advanced Technology Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/1/1978
Pages: 232
Contract: F33615-73-C-3051
Project: 8120
Task: 812016
AD Number: ADA067550
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Handling Quality Requirements for Advanced Aircraft Design: Longitudinal Mode
Report Number: AFFDL TR 78-154
Author(s): Ralph H. Smith; Norman D. Geddes
Corporate Author: Systems Research Laboratries, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1979
Pages: 184
Contract: F33615-77-C-3011
Project: 2090
Task: 209002
AD Number: ADA077858
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Proceedings of AFFDL Flying Qualities Symposium Held at Wright State University 12-15 September 1978
Report Number: AFFDL TR 78-171
Author(s): G. Thomas Black; David J. Moorhouse; Robert J. Woodcock
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 656
Contract: Laboratory Research - No Contract
Project: None Given
Task: None Given
AD Number: ADA066493
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Table of Contents
Report Number: AFFDL TR 78-171 p. i-vii
Author(s):
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 8
AD Number: See ADA066493
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Introduction
Report Number: AFFDL TR 78-171 p. 1-4
Author(s):
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 4
AD Number: See ADA066493
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Welcome and Introduction
Report Number: AFFDL TR 78-171 p. 5-7
Author(s): W. E. Lamar
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 3
AD Number: See ADA066493
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Opening Remarks
Report Number: AFFDL TR 78-171 p. 8-11
Author(s): R. A. Rushworth
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 4
AD Number: See ADA066493
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Introduction
Report Number: AFFDL TR 78-171 p. 12
Author(s): W. E. Lamar
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 1
AD Number: See ADA066493
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Remarks, Dr. W. R. Beam
Report Number: AFFDL TR 78-171 p. 13-22
Author(s): W. R. Beam
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 10
AD Number: See ADA066493
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Evaluation of Selected Class III Requirements of MIL-F-8785B (ASG), "Flying Qualities of Piloted Airplanes"
Report Number: AFFDL TR 78-171 p. 23-44
Author(s): Withers, C. C.
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 22
AD Number: See ADA066493
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Task-Oriented Flying Qualities for Air-to-Ground Gun Attack
Report Number: AFFDL TR 78-171 p. 45-57
Author(s): Brandeau, G.
Corporate Author: Fairchild Republic Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 13
AD Number: See ADA066493
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Longitudinal Maneuvering Control Characteristics of a Canard-Wing Fighter Configuration
Report Number: AFFDL TR 78-171 p. 58-87
Author(s): Cichy, Daniel R.
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 30
AD Number: See ADA066493
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Another Study of the T-38A PIO Incident
Report Number: AFFDL TR 78-171 p. 88-126
Author(s): Chalk, C. R.
Corporate Author: Calspan Advanced Technology Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 39
AD Number: See ADA066493
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High Angle of Attack Flying Qualities and Departure Criteria Development
Report Number: AFFDL TR 78-171 p. 127-152
Author(s): Hellman, Gary. K. and Robert B. Crombie
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 26
AD Number: See ADA066493
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Summary of Recent Handling Quality Results at STI Pertinent to Revision of MIL-F-8785B
Report Number: AFFDL TR 78-171 p. 153-175
Author(s): Hoh, Roger H. and Irving L. Ashkenas
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 23
AD Number: See ADA066493
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Flying Quality Requirements for the AMST
Report Number: AFFDL TR 78-171 p. 176-186
Author(s): Cerken, Gary J.
Corporate Author: Aeronautical Systems Division
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 11
AD Number: See ADA066493
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Impact of Key Flying Qualities Requirements on the YC-14/C-14 Design
Report Number: AFFDL TR 78-171 p. 187-202
Author(s): Carlson, E. Frank
Corporate Author: Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 16
AD Number: See ADA066493
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The Application of Equivalent Systems
Report Number: AFFDL TR 78-171 p. 203-218
Author(s): The Application of Equivalent Systems
Corporate Author: MCAIR
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 16
AD Number: See ADA066493
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Summary of Validation Efforts for MIL-F-8785B
Report Number: AFFDL TR 78-171 p. 219-235
Author(s): Browne, John T.
Corporate Author: Control Dynamics Branch, AF Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 17
AD Number: See ADA066493
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Discussion and Status of the Proposed Revision (1978) to MIL-F-8785B
Report Number: AFFDL TR 78-171 p. 236-259
Author(s): Moorhouse, David J. and Robert J. Woodcock
Corporate Author: AF Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 24
AD Number: See ADA066493
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Northrop Review of MIL-F-8785B Proposed Revisions
Report Number: AFFDL TR 78-171 p. 260-283
Author(s): Lockenour, J. L.
Corporate Author: Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 24
AD Number: See ADA066493
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AFFDL 1978 Flying Qualities Symposium and Workshop B-1 Experience Related to MIL-F-8785B* and Proposed Revisions
Report Number: AFFDL TR 78-171 p. 284-299
Author(s): Campbell, J. E.
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 16
AD Number: See ADA066493
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An Approach to Simplify the Specification of Low Speed Maneuvering Pitch Control Force
Report Number: AFFDL TR 78-171 p. 300-312
Author(s): Cichy, Daniel R.
Corporate Author: Rockwell International Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 13
AD Number: See ADA066493
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A Suggested Criterion for Piloted Heading Control
Report Number: AFFDL TR 78-171 p. 313-337
Author(s): Hoh, Roger H. and Irving L. Ashkenas
Corporate Author: Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 25
AD Number: See ADA066493
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Proposed Revision to the Lateral-Directional Coupling Requirements of MIL-F-8785
Report Number: AFFDL TR 78-171 p. 338-378
Author(s): Chalk, C. R.
Corporate Author: Calspan Advanced Technology Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 41
AD Number: See ADA066493
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Discussion of the Proposed Revision from a Design Standpoint
Report Number: AFFDL TR 78-171 p. 379-383
Author(s):
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 5
AD Number: See ADA066493
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Workshop Discussion of the Proposed Revision from a Flight Test and Operations Viewpoint
Report Number: AFFDL TR 78-171 p. 384-388
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 5
AD Number: See ADA066493
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Workshop discussion of the Proposed Revision from an Analytical Concepts and Methods Viewpoint
Report Number: AFFDL TR 78-171 p. 389-392
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 4
AD Number: See ADA066493
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An Evaluation of Sidestick Force/Deflection Characteristics on Aircraft Handling Qualities
Report Number: AFFDL TR 78-171 p. 393-413
Author(s): Smith, Stephen B.
Corporate Author: Air Force Flight Test Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 21
AD Number: See ADA066493
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Sift Pilot-in-the-Loop Handling Qualities Test and Analysis Techniques
Report Number: AFFDL TR 78-171 p. 414-435
Author(s): Twisdale, Thomas R.
Corporate Author: 6510 Test Wing/Flight Test Technology Branch
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 22
AD Number: See ADA066493
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Effects of Control System Dynamics on Fighter Approach And Landing Longitudinal Flying Qualities
Report Number: AFFDL TR 78-171 p. 436-470
Author(s): Smith, Rogers E.
Corporate Author: Calspan Advanced Technology Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 35
AD Number: See ADA066493
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The NT-33A Equivalent System Program (An Informal Report)
Report Number: AFFDL TR 78-171 p. 471-491
Author(s): Smith, Rogers E. and John Hodgkinson
Corporate Author: Calspan Advanced Technology Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 21
AD Number: See ADA066493
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Shuttle Orbiter Flight Control System Evaluation
Report Number: AFFDL TR 78-171 p. 492
Author(s): Brown, L. and M. Moul
Corporate Author: NASA/LaRC
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 1
AD Number: See ADA066493
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NASA/DFRC Evaluation of Digital Flight Control System Delays Using the DFCS F-8 Airplane
Report Number: AFFDL TR 78-171 p. 493-496
Author(s): Berry, Don and Bruce Powers
Corporate Author:
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 4
AD Number: See ADA066493
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Aeronautical Procurement - The Primary Specification System
Report Number: AFFDL TR 78-171 p. 497-512
Author(s): Weingarten, Joseph L.
Corporate Author: Aeronautical Systems Division
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 16
AD Number: See ADA066493
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Suggestions for the MIL-Prime-Standard Organization
Report Number: AFFDL TR 78-171 p. 513-521
Author(s): Carlson, Frank E.
Corporate Author: Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 9
AD Number: See ADA066493
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A New Approach to Quantification of Flying Qualities Excellence
Report Number: AFFDL TR 78-171 p. 522-544
Author(s): Wilson, Frank M.
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 23
AD Number: See ADA066493
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New Criteria for Advanced Flight Design
Report Number: AFFDL TR 78-171 p. 545-573
Author(s): Smith, Ralph H. and Norman D. Geddes
Corporate Author: Systems Research Laboratories, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 29
AD Number: See ADA066493
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Closed Loop Flying Qualities Criteria
Report Number: AFFDL TR 78-171 p. 574-586
Author(s): George, Frank L.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 13
AD Number: See ADA066493
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The MIL-PRIME-STD, Contents and Philosophy
Report Number: AFFDL TR 78-171 p. 587-590
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 4
AD Number: See ADA066493
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Advanced Aircraft Concepts and Controls
Report Number: AFFDL TR 78-171 p. 591-592
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 2
AD Number: See ADA066493
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High-Angle-of-Attack Criteria
Report Number: AFFDL TR 78-171 p. 593-602
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 10
AD Number: See ADA066493
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Flight Testing and Operations
Report Number: AFFDL TR 78-171 p. 603-604
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 2
AD Number: See ADA066493
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Pilot-in-the-Loop Criteria Development
Report Number: AFFDL TR 78-171 p. 605-610
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 6
AD Number: See ADA066493
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Summary and Concluding Remarks
Report Number: AFFDL TR 78-171 p. 611-622
Author(s):
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 12
AD Number: See ADA066493
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Appendix A: Flying Qualities Symposium Attendees
Report Number: AFFDL TR 78-171 p. 623-628
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Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 6
AD Number: See ADA066493
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Appendix B: AFFTC Parameter Identification Experience
Report Number: AFFDL TR 78-171 p. 629-648
Author(s): Maunder, David P
Corporate Author: Air Force Flight Test Center
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1978
Pages: 20
AD Number: See ADA066493
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Digital Computer Solution of Aircraft Longitudinal and Lateral-Directional Dynamic Characteristics
Report Number: AFFDL TR 78-203
Author(s): John M. Griffin; Robert B. Yeager; Larry B. Jordan; David A. Ratino
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1979
Pages: 172
Contract: Laboratory Research - No Contract
Project: None Given
Task: None Given
AD Number: ADA078672
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