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Inversion of the Prandtl-Meyer relation
Published online by Cambridge University Press: 04 July 2016
Summary
A simple rational fraction is derived which gives the Mach number with an error of less than 0·05 per cent for a given value of the Prandtl-Meyer function.
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- Technical note
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- Copyright
- Copyright © Royal Aeronautical Society 1975
References
1.
Fraser, S. M.
Calculation of Mach number from given turning angle in supersonic isentropic flow. The Aeronautical Journal, Vol 79, No 770, pp 95–96, February 1975.Google Scholar
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