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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
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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., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-128
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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, Daniel
Corporate 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, Frank
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TR 61-60 Part 2
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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, Jarvis
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TDR 62-171
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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
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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., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
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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, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
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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, Lawrence
Corporate 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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