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27 items
![FDLTDR64-007.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/7e275e7f2d222d545d8b6bfe5cd193c99ad32647.jpg)
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The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations
Author(s): Brook, John W.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report number: FDL TDR 64-7
![FDLTDR64-128.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/415f7b485af6e9dfae6f5094b83faa14bb6a174e.jpg)
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Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Evans, William J., Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-128
![ASDTDR62-168.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/68bdd2a9eb5ec83295c268df48c68a2abb49552a.jpg)
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A Review of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., Oman, Richard A., Hartofilis, Stavros A., Meckler, Lawrence H., Evans, William J., Weiss, DanielCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-03
Report number: ASD TDR 62-168
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An Investigation of Magnetohydrodynamic Principles Applicable to Flight Control
Author(s): Ericson, William B., Maciulaitis, Algirdas, Spagnolo, Frank A., Loeffler, Albert L., Scheuing, Richarde A., Hopkins, Harold B.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-12
Report number: ASD TDR 62-649
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Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8
Author(s): Mead, Harold R., Koch, FrankCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TR 61-60 Part 2
![ASDTDR62-171.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/ab28631ec5ad18ea0a0737f289f80dbfbdb0ea00.jpg)
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Investigation of Pressure Distributions Over Planar, Twisted, and Cambered Wings in a Hypersonic Shock Tunnel
Author(s): Scheuing, Richard A., Leng, JarvisCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TDR 62-171
![FDLTDR64-082.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/13bd1f420f4b6a923570eafa77e0710ea418d867.jpg)
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A Conical Thin-Shock-Layer Theory Uniformly Valid in the Entropy Layer
Author(s): Melnik, Robert E.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: FDL TDR 64-82
![FDLTDR64-120.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e2f97563261c3377ff91085a130db63b7ebd0077.jpg)
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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
![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
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- Kaufman, Louis G. (6)
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