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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Format: | Government Document Book |
Language: | English |
Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4125. |
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Call Number: |
Y 3.N 21/5:6/4125
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Y 3.N 21/5:6/4125 | Available Place a Hold |