Investigation of Laminar Aerodynamic Heat-Transfer Characteristics of Hemisphere-Cylinder in Langley 11-Inch Hypersonic Tunnel at Mach Number of 6.8.
Investigation of laminar aerodynamic heat-transfer characteristics of hemisphere-cylinder in Langley 11-inch hypersonic tunnel at mach number of 6.8
NACA -- Tech Note
1956
38 pages
Report
English
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