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Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration
Author(s): Kaufman, Louis G., IICorporate 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
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Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Author(s): None GivenCorporate Author(s): Bendix Corp Southfield Mich
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-03
Report number: FDL TDR 64-32 Final Report
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Application Of High Moment-Producing Techniques For Control Of A Manned Space Vehicle
Author(s): None GivenCorporate 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
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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
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Analytical and Experimental Investigation of Coated Metal Fabric Expandable Structures for Aerospace Applications
Author(s): None GivenCorporate Author(s): Goodyear Aerospace Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report number: ASD TDR 63-542
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Investigation of a Close Tolerance Pyrotechnic Metallic Delay Element
Author(s): Peterson, W. R.Corporate Author(s): Frankford Arsenal
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-563
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Low Frequency Instabilities of Free Systems
Author(s): Schwendler, Robert G., Hill, Jack H.Corporate Author(s): Computer Engineering Associates
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report number: ASD TDR 63-655
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Structural Design for Acoustic Fatigue
Corporate Author(s): Douglas Aircraft CompanyLaboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-10
Report number: ASD TDR 63-820
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Automatic Runway Profile Measuring Instrumentation And Runaway Properties. Part III: Base Surveys
Author(s): Turner, D. F.Corporate Author(s): Midwest Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report number: WADD TR 60-470 Part III
full text available
Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: RTD TDR 63-4044 Part 3
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