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Download or read book Investigation of the Laminar Aerodynamic Heat transfer Characteristics of a Hemisphere cylinder in the Langley 11 inch Hypersonic Tunnel at a Mach Number of 6 8 written by Davis H. Crawford and published by . This book was released on 1956 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt: At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.

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