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75 items
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Asymptotic Stability of Equilibrium of a Simplified Aerodynamic Vehicle with Flexible Tail
Author(s): Wang, P. K. C.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 65-71
full text available
Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method
Author(s): Wang, P. K. C.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 72-83
full text available
Optimum Control of a Class of Mixed Distributed and Lumped Parameter Systems
Author(s): Wang, P. K. C.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 84-106
full text available
Estimates for Truncation Errors of Infinite Dimensional Systems of Linear Ordinary Differential Equations
Author(s): Brady, M. L., Wang, P. K. C.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 107-126
full text available
An Improved Estimate for the Error of Truncation for an Infinite System of Ordinary Differential Equations
Author(s): Brady, M. L.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 127-140
full text available
Theory of Stability and Control for Distributed Parameter Systems. An Annotated Bibliography
Author(s): Wang, P. K. C.Corporate Author(s): IBM San Jose Research Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11-01
Report number: AFFDL TR 65-145 p. 141-164
full text available
Development of Subsonic Base Pressure Prediction Methods
Author(s): Butsko, J. E., Carter, W. V., Herman, W.Corporate Author(s): GD/Convair, General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-09
Report number: AFFDL TR 65-157 Volume 2
full text available
Development of Subsonic Base Pressure Prediction Methods
Author(s): Butsko, J. E., Carter, W. V., Herman, W.Corporate Author(s): GD/Convair, General Dynamics Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-09
Report number: AFFDL TR 65-157 Volume 1
full text available
Skin Friction, Heat Transfer, and Pressure Measurements on Hypersonic Inlet Compression Surfaces in the Mach Number Range 7.5 to 16
Author(s): Ryder, M. O., Jr.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-12
Report number: AFFDL TR 65-199
full text available
Application of Pilot-Controller Integration Techniques to a Representative V/STOL Aircraft
Author(s): Gaul, John W.Corporate Author(s): Bell Aerosystems Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-10
Report number: AFFDL TR 65-200
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