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Second Test Region Of A Free-jet Supersonic wind Tunnel As A Region Of Variable Mach Number
Author(s): Lee, J. D., Von Eschen, G. L.Corporate Author(s): Aerodynamic Laboratory, Dept. Of Aeronautical Engineering, Ohio State University.
Date of Publication: 1956-06
Report number: WADC TR 56-337
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. I. Surface Pressure Distributions on a Blunted Flat Plate
Author(s): Gregorek, G. M., Nark, T. C., Lee, J. D.Corporate Author(s): Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report number: ASD TDR 62-792 Volume 1
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. II. Laminar Boundary Layer Profile on the Flat Plate
Author(s): Gregorek, G. M., Nark, T. C., Lee, J. D.Corporate Author(s): Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report number: ASD TDR 62-792 Volume 2
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