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Evaluation of the Flying Qualities Requirements of MIL-F-8785B(ASG) Using the C-5A Airplane
Report Number: AFFDL TR 75-3
Author(s): Charles L. Silvers; Clifton C. Withers
Corporate Author: Lockheed-Georgia Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 3/20/1975
Pages: 333
Contract: F33615-75-C-3012
Project: None Given
Task: None Given
AD Number: ADA011728
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The Effects of Mass Transfer and Angle of Attack on Hypersonic Turbulent Boundary Layer Characteristics
Report Number: AFFDL TR 75-35
Author(s): A. L. Laganelli; R. P. Fogaroli; A. Martellucci
Corporate Author: General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1975
Pages: 155
Contract: F33615-74-C-3016
Project: 1366
Task: None Given
AD Number: ADA012700
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Flight Investigation of Fighter Side-Stick Force-Deflection Characteristics
Report Number: AFFDL TR 75-39
Author(s): G. Warren Hall; Roger E. Smith
Corporate Author: Calspan Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 5/1/1975
Pages: 92
Contract: F33615-73-C-3051
Project: 8219
Task: None Given
AD Number: ADA013926
Photo Enhancement: Complete
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Human factors Evaluation of Several Control System Configurations Including Work Load Sharing with Force Wheel Steering During Approach and Flare
Report Number: AFFDL TR 75-43
Author(s): Mark S. Crabtree
Corporate Author: Systems Research Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 4/1/1975
Pages: 102
Contract: F33615-74-C-3050
Project: 8226
Task: 822601
AD Number: ADA014836
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Application of Differential Games to Air-to-Air Combat Problems
Report Number: AFFDL TR 75-47
Author(s): L. Earl Miller
Corporate Author: High Speed Aero Perfomance Branch
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1975
Pages: 181
Contract: Laboratory Research - No Contract
Project: 1366
Task: 136602
AD Number: ADA017034
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Abstract Text:
Differential game barrier theory was applied to three pursuit-evasion problems. For the first problem the solution involving the angle-off constraint was directly determined from the natural barrier solution. For the second problem the capture range was relatively insensitive to the angle-off. The solution to the third problem which approximates the terminal part of air-to-air combat showed that an increase in the pursuer's speed or a decrease in his minimum radius of turn resulted in a decrease in the capture range.
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Low Visibility Landing Pilot Modeling Experiment and Data, Phase II
Report Number: AFFDL TR 75-57
Author(s): R. Gressang
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1975
Pages: 222
Contract: Laboratory Research - No Contract
Project: 2187
Task: 218702
AD Number: ADA016764
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The Effects of Stability Augmentation on the Gust Response of a STOL Aircraft During a Curved Manual Approach
Report Number: AFFDL TR 75-63
Author(s): Milton B. Porter
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 6/1/1975
Pages: 228
Contract: Laboratory Research - No Contract
Project: 8219
Task: None Given
AD Number: ADA014301
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Dot Matrix Display Symbology Study
Report Number: AFFDL TR 75-72
Author(s): R. J. Vanderkolk; J. A. Herman; M. L. Hershberger
Corporate Author: Hughes Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1975
Pages: 199
Features: + Diagram(s) + Graph(s) + Table(s)
Contract: F33615-74-C-3065
Project: 2020
Task: 20200007
AD Number: ADA016470
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Abstract Text:
This report describes a concentrated effort to identify and quantify the parameters involved in the design of matrix displays for legibility and to assess the design trade-offs against the criterion of symbol legibility. A literature survey was conducted to determine what information previously existed and its applicability to matrix displays. The literature survey is included as an appendix to this report.
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All Digital Simulation for Manned Flight in Turbulence
Report Number: AFFDL TR 75-82
Author(s): Joseph J. Pollard
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 9/1/1975
Pages: 190
Contract: Laboratory Research - No Contract
Project: None Given
Task: None Given
AD Number: ADA018126
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Experimental and Theoretical Control Surface Characteristics on Low Aspect Ratio Delta Wing Vehicles at Subsonic Mach Numbers
Report Number: AFFDL TR 75-90
Author(s): Peter R. Gord
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1975
Pages: 146
Contract: Laboratory Research - No Contract
Project: 1366
Task: 136601
AD Number: ADA023408
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Small Disturbance Transonic Flows About Oscillating Airfoils and Planar Wings
Report Number: AFFDL TR 75-100
Author(s): R. M. Traci; E. D. Albano; J. L. Farr, Jr.
Corporate Author: Science Applications, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 8/1/1975
Pages: 165
Contract: F33615-74-C-3094
Project: 1370
Task: 137004
AD Number: ADB008124
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Further Investigations of the Near Field Trailing Vorticity Behind a STOL Aircraft
Report Number: AFFDL TR 75-132
Author(s): Lawrence J. Mertaugh; Krishna Devarayalu
Corporate Author: Mississippi State University
Laboratory: Air Force Flight Dynamics Laboratory
Publication Date: 12/1/1975
Pages: 49
Contract: F33615-74-C-3066
Project: 1929
Task: 192903
AD Number: ADA035685
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Active Control Synthesis for Flexible Vehicles: Volume I. KONPACT Theoretical Description
Report Number: AFFDL TR 75-146 Volume 1
Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1976
Pages: 300
Contract: F33615-75-C-3046
Project: 8219
Task: 821902
AD Number: ADB015198
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Active Control Synthesis for Flexible Vehicles: Volume II. KONPACT Program Listing
Report Number: AFFDL TR 75-146 Volume 2
Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1976
Pages: 326
Contract: F33615-75-C-3046
Project: 8219
Task: 821902
AD Number: ADB015216
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Active Control Synthesis for Flexible Vehicles: Volume III. KONPACT User's Manual
Report Number: AFFDL TR 75-146 Volume 3
Author(s): A. F. Konar; J. K. Mahesh; C. R. Stone; M. Hank
Corporate Author: Honeywell Systems & Research Center
Laboratory: U. S. Air Force Flight Dynamics Laboratory
Publication Date: 7/1/1976
Pages: 262
Contract: F33615-75-C-3046
Project: 8219
Task: 821902
AD Number: ADB015025
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