Abstract
Hypersonic flows around axisymmetrical power-law slender bodies are calculated for high, but finite, Mach numbers, and for low angles of attack. This is done by a small-perturbation expansion of self-similar solutions using the equivalence principle. The stream functions are found and a solidification principle is used in order to define hypersonic aircrafts.
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© 1994 Springer
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Merlen, A. (1994). From the analytical theory to hypersonic aircraft design. In: Bois, PA., Dériat, E., Gatignol, R., Rigolot, A. (eds) Asymptotic Modelling in Fluid Mechanics. Lecture Notes in Physics, vol 442. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-59414-0_69
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DOI: https://doi.org/10.1007/3-540-59414-0_69
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