Investigation of boundary-layer transition on 10 degree cone in Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 / Archibald R. Sinclair anbd K.R. Czarnecki.

An investigation has been made to determine the transition Reynolds numbers on a 10 degree cone in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 and over a Reynolds number range from about 800,000 to 9,500,000 per foot. The results indicate that, on the...

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Bibliographic Details
Main Author: Sinclair, Archibald R.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Czarnecki, K. R.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3648.
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Call Number: Y 3.N 21/5:6/3648
Y 3.N 21/5:6/3648 Available Place a Hold