Search

64 items

application/pdf thumbnail
full text available
Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
application/pdf thumbnail
full text available
Pressure Measurements at Mach 8 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
application/pdf thumbnail
full text available
Heat Transfer Measurements at Mach 9 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-142
full text by request
Digital Adaptive Flight Control System Phase II
Author(s): Andeen, R. E., Shipley, P. P.
Corporate Author(s): Sperry Phoenix Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-854
full text by request
Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: RTD TDR 63-4179 Part 1
application/pdf thumbnail
full text available
Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Author(s): None Given
Corporate Author(s): Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Report number: FDL TDR 64-32 Final Report
application/pdf thumbnail
full text available
Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Author(s): None Given
Corporate Author(s): Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Report number: FDL TDR 64-32 Summary Final Report
full text by request
Demonstration of the Application of Majority Logic for Increased Reliability in Automatic Flight Control Systems
Author(s): Derby, R. M., Fleck, J. J.
Corporate Author(s): General Electric Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report number: ASD TDR 63-275
full text by request
A Measurement of the Static Aeroelastic Deformation and Loading of a Wing in Supersonic Flow
Author(s): Durgin, F. H., Bartlett, C. J.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-366
full text by request
Analytical and Experimental Investigation of Coated Metal Fabric Expandable Structures for Aerospace Applications
Author(s): None Given
Corporate Author(s): Goodyear Aerospace Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report number: ASD TDR 63-542

Refine your search

Refine your search