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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 VII - Velocity Potentials in Non-Uniform Transonic Flow Over a Thin Wing
Author(s): Andrew, L. V., Stenton, T. E.Corporate Author(s): North American Rockwell Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-08
Report number: FDL TDR 64-152 Part 7
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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
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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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