Search

649 items

application/pdf thumbnail
full text available
Fixed-Base and In-Flight Simulations of Longitudal and Lateral-Directional Handling Qualities for Piloted Re-Entry Vehicles
Author(s): Kidd, Edwin A., Harper, Robert P., Jr.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: ASD TDR 61-362
full text unavailable
Research and Development of a Hot Gas Flight Stabilization System
Author(s): Feucht, R. E., Taplin, L. B., Bosworth, R., Gregory, A., MacArthur, G.
Corporate Author(s): Bendix Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: WADD TR 60-449 Part IV
application/pdf thumbnail
full text available
Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Problem Formulation
Author(s): Brown, Robert C., Brulle, Robert V., Combs, A. E., Griffin, Gerald D.
Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-1 Part 1 Volume 1
full text by request
Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report number: RTD TDR 63-4239
application/pdf thumbnail
full text available
An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II, Meckler, Lawrence, Hartofilis, Stavros A., Weiss, Daniel
Corporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: AFFDL TR 64-174
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part I: Pressure Data for Delta Wing Surface
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report number: FDL TDR 64-2 Part 1

Refine your search

Refine your search