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Empirical Correlation of Excitation Environment and Structural Parameters with Flight Vehicle Vibration Response
Author(s): White, R. W., Bozich, D. J., Eldred, K. M.
Corporate Author(s): Northrup Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: AFFDL TR 64-160
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Extension of Linear Constant-Coefficient Analysis Methods to Time-Varying Systems
Author(s): Johnson, Walter A., McRuer, Duane T., Phatak, Anil V.
Corporate Author(s): Systems Technology, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: RTD TDR 63-4178
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Altimeter Display Study Part I. Summary and Review of Data Requirements
Author(s): Matheny, W. G.
Corporate Author(s): Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-621 Part 1
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Altimeter Display Study Part II. Handbook for Static Testing of Altimeters
Author(s): Elam, C. B., Matheny, W. G., Schum, D. A.
Corporate Author(s): Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-622 Part 2
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Altimeter Display Study Part III. Summary of Experimental Testing
Author(s): Elam, C. B., Matheny, W. G., Schum, D. A.
Corporate Author(s): Bell Helicopter Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: ASD TDR 63-623 Part 3
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The Effect of Surface Perturbations on the Pressure Distributions About Blunt Two-Dimensional Bodies at High Mach Numbers
Author(s): Donaldson, Coleman duP., Sullivan, Roger D., Hayes, Wallace D.
Corporate Author(s): Aeronautical Research Associates of Princeton, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: FDL TDR 64-17
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Preliminary Design Considerations for a V/STOL Wind Tunnel
Author(s): Knowlton, Marcus P.
Corporate Author(s): Princeton University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: FDL TDR 64-146
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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
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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., 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
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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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