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Distinctive features of the transonic flow behind the trailing corner edge of an oversized cone-cylinder body

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Abstract

The results of an experimental study of the transonic flow behind the trailing corner edges of oversized cone-cylinder bodies of different dimensions are presented. Emphasis is placed on the induced transonic flow restructuring and the local aerodynamic forces accompanying the process, both steady and unsteady. The restructuring that occurs with increase in the freestream Mach number is studied.

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Authors
  1. B. N. Dan'kov
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  2. A. P. Kosenko
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  3. V. N. Kulikov
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  4. V. N. Otmennikov
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Additional information

Original Russian Text © B.N. Dan'kov, A.P. Kosenko, V.N. Kulikov, V.N. Otmennikov, 2007, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2007, Vol. 42, No. 3, pp. 155–168.

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Dan'kov, B.N., Kosenko, A.P., Kulikov, V.N. et al. Distinctive features of the transonic flow behind the trailing corner edge of an oversized cone-cylinder body. Fluid Dyn 42, 472–484 (2007). https://doi.org/10.1134/S0015462807030155

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  • DOI: https://doi.org/10.1134/S0015462807030155

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