Effects of nose angle and Mach number on transition on cones at supersonic speeds / K.R. Czarnecki and Mary W. Jackson.
An investigation has been made to determine the transition characteristics of a group of smooth, sharp-nosed cones varying from 10 degrees to sixty degrees in included apex angle over a Mach number range from 1.61 to 2.20 and a range of Reynolds number per foot from about 1.5 million to 8 million. I...
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Format: | Government Document Book |
Language: | English |
Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4388. |
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Call Number: |
Y 3.N 21/5:6/4388
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Y 3.N 21/5:6/4388 | Available Place a Hold |