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A Study of Conventional Airplane Handling Qualities Requirements: Part II. Lateral-Directional Oscillatory Handling Qualities
Author(s): Ashkenas, I. L.
Corporate Author(s): Systems Technology, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-11
Report number: AFFDL TR 65-138 Part 2
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Unsteady Aerodynamics for Advanced Configurations: Part III - Elliptic-Conical Wing in Linearized Unsteady Transonic Flow
Author(s): Albano, E., Andrew, L. V.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05
Report number: FDL TDR 64-152 Part 3
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Research Program for a Single-Axis, Triple-Redundant, Self-Adaptive Flight-Control System Utilizing Integrated Circuits
Author(s): Shemeta, E.
Corporate Author(s): Fairchild Space and Defence Systems
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: FDL TDR 64-139
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An Evaluation of Procedures for Calculating Aerodynamic Loads
Author(s): Schindel, Leon H.
Corporate Author(s): Massachusetts institute of Technology
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05
Report number: AFFDL TR 65-18
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Table of Contents
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. i-iv
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Introduction
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. 1-4
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Application of Lyapunov's Direct Method to Stability Problems in Elastic and Aeroelastic 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. 29-64
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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
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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
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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

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