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Maximum turning angles of a supersonic flow in shock-wave systems

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Abstract

The possibility of creating shock-wave systems to achieve maximum supersonic flow turning angles is considered. The relation between these systems and both geometrically conditioned optimal systems and the shock-wave structures formed as a result of interaction between gasdynamic discontinuties is investigated.

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Authors
  1. A. V. Omel’chenko
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  2. V. N. Uskov
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Additional information

St. Petersburg. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 3, pp. 148–156, May–June, 1998.

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Omel’chenko, A.V., Uskov, V.N. Maximum turning angles of a supersonic flow in shock-wave systems. Fluid Dyn 33, 419–426 (1998). https://doi.org/10.1007/BF02698194

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  • DOI: https://doi.org/10.1007/BF02698194

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