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![AFFDLTR64-174.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d721bef1c3be61914c70f8a284ee2e4969dbf421.jpg)
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An Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II, Meckler, Lawrence, Hartofilis, Stavros A., Weiss, DanielCorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: AFFDL TR 64-174
![FDLTDR64-124.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/69a5f060718a68abae188670a0eca41ea12ef330.jpg)
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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, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
![FDLTDR64-142.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/c2d9448d1bacdaaff536bdccde11aec4552b4694.jpg)
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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, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-142
![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
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Pressure and Heat Transfer Measurements at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-235
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