Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 / by Ivan E. Beckwith and James J. Gallagher.

An investigation was made of the pressure and equilibrium-temperature distributions on sphere at Mach numbers of 2.00 and 4.15. The local aerodynamic best transfer was also measured on a sphere at a Mach number of 2.00 and on a hemisphere-cylinder at a Mach number of 4.15. The Reynolds number range...

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Bibliographic Details
Main Author: Beckwith, Ivan E.
Corporate Authors: Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Other Authors: Gallagher, James J.
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 4125.
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Call Number: Y 3.N 21/5:6/4125
Y 3.N 21/5:6/4125 Available Place a Hold