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Development and Flight Calibration of a Variable-Drag Device on a Variable Stability T-33 Airplane
Author(s): Newell, F. D., Dolbin, B. H., Schelhorn, A. E.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report number: ASD TDR 62-910
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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
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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 Given
Corporate 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 Company
Laboratory: 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
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Static Aerodynamic Characteristics at Mach 5 and 8 of 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: 1963-09
Report number: FDL TDR 64-10
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Design Criteria For Ground-Induced Dynamic Loads
Author(s): Hahn, Edward E.
Corporate Author(s): IIT Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report number: RTD TDR 63-4139 Volume 1

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