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64 items
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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
![ASDTDR63-655.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/62df9592e5922053a5591f8202b6d86df4228b0c.jpg)
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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
![ASDTDR63-820.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/b35bd9b18693bd19efd6a5b7bc980d31661176fe.jpg)
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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
![RTDTDR63-4044part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f186fe454b7ad3b01fb8222af483ca7fe32ac304.jpg)
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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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Three-Degree-of-Freedom Problem Optimization Formulation Volume 3 - User's Manual
Author(s): Mobley, R. L., Vorwald, R. F.Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-06
Report number: FDL TDR 64-1 Part 2 Volume 3
![FDLTDR64-010.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/9b381f18ecd0bc9349d091807eefecc1e718f0e6.jpg)
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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, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: FDL TDR 64-10
![FDLTDR64-016part01volume01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/86fae0c818e8ea1f4946a17596d7b68395117c07.jpg)
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Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume I, Aerodynamics
Author(s): Batt, James R.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-16 Part 1 Volume 1
![FDLTDR64-016part01volume02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/9f3c04a1fc0c2908f4d05576b1ae0e159826958a.jpg)
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Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics
Author(s): Batt, James R.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-16 Part 1 Volume 2
![FDLTDR64-016part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e5fd08e59bb3ea6018534f1b8e9fe07f7ff0f70c.jpg)
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Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity
Author(s): Batt, James R., Gallagher, Richard H.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-16 Part 2
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