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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
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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 1
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Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hartofilis, Stavros A.Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Date of Publication: 1963-05
Report number: ASD TDR 63-319
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Experimental Investigation of Pressures on a Blunt Two-Dimensional Profile and on Sharp and Blunt Conical Shapes of Noncircular Cross Section 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: 1963-08
Report number: ASD TDR 63-169
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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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Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity
Author(s): Gilmore, Arthur, Seredinsky, Vladimir, MacKenzie, DonaldCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 62-460
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- Kaufman, Louis G. (2)
- Koch, Frank (2)
- Mead, Harold R. (2)
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- Gilmore, Arthur (1)
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- Hopkins, Harold B. (1)
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- Spagnolo, Frank A. (1)
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