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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 1998, Volume 39, Issue 5, Pages 116–121
(Mi pmtf3320)
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Three-dimensional supersonic flow around a pointed body with upstream energy supply
T. A. Korotaeva, V. M. Fomin, A. P. Shashkin Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090
Abstract:
The effect of a local source of energy on a three-dimensional supersonic flow and the aerodynamic characteristics of a pointed ogival body is numerically studied. The results obtained show that the position of the local source of energy upstream of the body on the axis or its deviation from the axis can affect significantly the aerodynamic characteristics of the body (drag, lift, and pitching moment) and the flight trajectory of the vehicle.
Received: 30.12.1996 Accepted: 13.02.1997
Citation:
T. A. Korotaeva, V. M. Fomin, A. P. Shashkin, “Three-dimensional supersonic flow around a pointed body with upstream energy supply”, Prikl. Mekh. Tekh. Fiz., 39:5 (1998), 116–121; J. Appl. Mech. Tech. Phys., 39:5 (1998), 753–757
Linking options:
https://www.mathnet.ru/eng/pmtf3320 https://www.mathnet.ru/eng/pmtf/v39/i5/p116
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Abstract page: | 29 | Full-text PDF : | 7 |
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