Supersonic ideal-gas flow of in the throat region of a nozzle

DOI10.1007/BF02030229zbMath0875.76195MaRDI QIDQ1354763

S. V. Yagudin

Publication date: 9 November 1997

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

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (2)

Inviscid gas flows in nozzles with a steeply converging contour ⋮ Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line

Cites Work

• Transonic flow in the throat region of axisymmetric nozzles
• Unnamed Item

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