Calculation of base pressure and enthalpy behind a blunt trailing edge separating two supersonic streams with allowance for boundary layers and heat fluxes

DOI10.1007/BF01051001zbMath0800.76223MaRDI QIDQ1315637

V. K. Masalov, R. K. Tagirov

Publication date: 20 March 1994

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

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (1)

Determination of the optimal contour of a supersonic jet engine outlet by the direct method

Cites Work

• Unnamed Item
• A second-order finite-difference scheme for computing three-dimensional supersonic flows of an ideal gas
• Supersonic Axisymmetric Flow over Boattails Containing a Centered Propulsive Jet

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