Gasdynamics active channel amplifier supersonic jet management position airframe

Authors

  • Ernst Gaysovich Gimranov
  • Anton Vyacheslavovich Svistunov

Keywords:

supersonic power; the posi tion of the body of the aircraft; the supersonic flow of gas; a pseudo- shock.

Abstract

The article considers the problem of calculation and analysis of the flow parameters change in one-dimensional steady-state currents without penetration into the mechanism of the phenomenon, gas-dynamic flow structure in the pseudo-shock. The flow of a pseudo-shock in a weakly widening profiled supersonic jetactive channel amplifier, and the influence on it.

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Published

2018-03-10

Issue

Vol. 17 No. 1 (54) (2013): Вестник УГАТУ

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY