Inviscid gas flows in nozzles with a steeply converging contour

DOI10.1134/S0015462812020093zbMath1242.76093MaRDI QIDQ431754

S. V. Yagudin

Publication date: 2 July 2012

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

characteristicschockingcontouringinviscid gasnozzles

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Related Items (1)

Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line

Cites Work

• Supersonic ideal-gas flow of in the throat region of a nozzle
• Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction
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