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Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack
Author(s): Li, T. C.
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 5
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Unsteady Aerodynamics for Advanced Configurations: Part IV - Application of the Supersonic Mach Box Method to Intersecting Planar Lifting Surfaces
Author(s): Moore, M. T., 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 4
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Unsteady Aerodynamics for Advanced Configurations: Part II - A Transonic Box Method for Planar Lifting Surfaces
Author(s): Rodemich, E. R., 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 2
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Unsteady Aerodynamics for Advanced Configurations: Part I - Application of the Subsonic Kernel Function to Nonplanar Lifting Surfaces
Author(s): Vivian, H. T., Andrews, 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 1
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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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Dynamics of Shell-Like Lifting Bodies: Part I. The Analytical Investigation
Author(s): Hung, F. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: AFFDL TR 65-17 Part 1
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Transient Dynamic Response of Orbiting Space Stations
Author(s): Tai, C. L., Andrew, L. V., Loh, M. M. H., Kamrath, P. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-25