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A Study of the Effects of Parameter Variation on the Flying Qualities of the XV-4B V/STOL Aircraft
Author(s): Jones, Arthur G.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-03
Report number: AFFDL TR 72-44
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An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition
Author(s): Kurylowich, George, Martin, James M.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-02
Report number: AFFDL TR 72-37
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The Design of Stability Augmentation Systems for Decoupling Aircraft Responses
Author(s): Pope, Rhall E.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-06
Report number: AFFDL TR 72-63
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An Analytical and Experimental Investigation of Hypersonic Viscous Interaction Pressure Effects
Author(s): Sliski, Neil J.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report number: AFFDL TR 73-58
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The Response of Aircraft Encountering Aircraft Wake Turbulence
Author(s): Nelson, Robert C.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1974-06
Report number: AFFDL TR 74-29
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Review of Methods of Solution of Afterbody/Exhaust Nozzle Flow Fields
Author(s): Calarese, WladimiroCorporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1974-01
Report number: AFFDL TR 74-108
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The Numerical Solution of the Asymptotic Equations of Trailing Edge Flow
Author(s): Jobe, Charles E.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1974-10
Report number: AFFDL TR 74-46
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The Effects of Stability Augmentation on the Gust Response of a STOL Aircraft During a Curved Manual Approach
Author(s): Porter, Milton B.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-06
Report number: AFFDL TR 75-63
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Low Visibility Landing Pilot Modeling Experiment and Data, Phase II
Author(s): Gressang, R.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-08
Report number: AFFDL TR 75-57
full text available
Experimental and Theoretical Control Surface Characteristics on Low Aspect Ratio Delta Wing Vehicles at Subsonic Mach Numbers
Author(s): Gord, Peter R.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-12
Report number: AFFDL TR 75-90
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