Plane contours with maximum thrust in a non-isentropic flow

Plane tasks of the contour and maximum thrust nozzle modelling in the supersonic flow with shock waves are formulated and solved analytically and numerically. The first of the considered problems relates to the optimal profiling of the tail part of the body. This part consists of some corner point,...

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Veröffentlicht in:	Journal of physics. Conference series 2018-11, Vol.1129 (1), p.12026
Hauptverfasser:	Mustaev, A R, Ostapenko, N A
Format:	Artikel
Sprache:	eng
Schlagworte:	Conical nozzles Contours Exact solutions Mathematical models Numerical methods Optimization Shock waves Supersonic flow Supersonic nozzles
Online-Zugang:	Volltext
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