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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2003, Volume 44, Issue 5, Pages 46–55
(Mi pmtf2536)
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This article is cited in 5 scientific papers (total in 5 papers)
Experimental study of supersonic flow around truncated cones at incidence
M. D. Brodetsky, A. M. Shevchenko Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
Abstract:
Results of an experimental study of supersonic flow around truncated cones with cone half-angles of $20$, $30$, and $40^\circ$, performed at Mach numbers $\mathrm{M}= 2, 3$, and $4$ within the range of angles of attack up to $20^\circ$, are presented. A relationship is established between the emergence of an internal shock wave and the character of pressure distribution along the generatrix of the truncated cone. It is shown that the known boundaries of regimes obtained for axisymmetric flow around sharp and blunt cones can be used to predict flow regimes in the vertical plane of symmetry of the truncated cone at incidence.
Keywords:
truncated cone, supersonic flow regimes, shock wave.
Received: 02.10.2001 Accepted: 21.01.2003
Citation:
M. D. Brodetsky, A. M. Shevchenko, “Experimental study of supersonic flow around truncated cones at incidence”, Prikl. Mekh. Tekh. Fiz., 44:5 (2003), 46–55; J. Appl. Mech. Tech. Phys., 44:5 (2003), 640–647
Linking options:
https://www.mathnet.ru/eng/pmtf2536 https://www.mathnet.ru/eng/pmtf/v44/i5/p46
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