S. A. Isaev, J. M. Lipnickii, A. N. Mikhalev, A. V. Panasenko, P. A. Baranov, “Simulation of reducing the drag of a Soyuz-type missile's reentry vehicle with a coaxial disk placed in front of it”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 2013, Volume 39, Issue 16,Pages <nobr>80

This article is cited in 3 papers

Simulation of reducing the drag of a Soyuz-type missile's reentry vehicle with a coaxial disk placed in front of it

S. A. Isaev^abc, J. M. Lipnickii^abc, A. N. Mikhalev^abc, A. V. Panasenko^abc, P. A. Baranov^abc

^a Saint-Petersburg State University of Civil Aviation
^b The Central Research Institute of Machinery, Korolev, Moscow region
^c Ioffe Institute, St. Petersburg

Abstract: The effect of a considerable reduction in the drag of the reentry vehicle of a Soyuz-type missile with a small-sized disk placed in front of it is grounded on the solution by a factorized finite-volume approach of the Navier–Stokes and Reynolds equations, closed in the latter case by a modified Menter shear-stress transport model considering the curvature of the streamlines.

Received: 12.03.2013