Hypersonic interaction of the vortex trail behind the wing and body of revolution with a shock wave at the inlet to the model air intake

Andrey M. Shevchenko; Andrey S. Shmakov; Ivan N. Kavun

Hypersonic interaction of the vortex trail behind the wing and body of revolution with a shock wave at the inlet to the model air intake

Andrey M. Shevchenko

1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation

shevch@itam.nsc.ru

Andrey S. Shmakov

1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation

2. Novosibirsk State University Novosibirsk, Russian Federation

shmakov@itam.nsc.ru

Ivan N. Kavun

1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation

i_k@list.ru

Zapryagaev V.I.

The material was received by the Editorial Board: 12.10.2007

УДК 533.06

Hypersonic interaction of the vortex trail behind the wing and body of revolution with a shock wave at the inlet to the model air intake

References: Shevchenko A.M., Shmakov A.S., Kavun I.N., Zapryagaev V.I. Hypersonic interaction of the vortex trail behind the wing and body of revolution with a shock wave at the inlet to the model air intake. Vestnik NSU. Series: Physics. 2007, vol. 2, no. 4. P. 38–44 (in Russ.). DOI: 10.54238/1818-7994-2007-2-4-38-44