Effect of energy release in shock layer on supersonic flight

DOI10.1007/BF01049872zbMath0729.76045OpenAlexW4249166640MaRDI QIDQ806474

S. I. Arafajlov

Publication date: 1990

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

Full work available at URL: https://doi.org/10.1007/bf01049872

zbMATH Keywords

supersonic flowshock wavemaximizationaxisymmetric bodycontrolling forceenergy release zone

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Related Items (1)

Reflection of disturbances produced by a three-dimensional heat source from a plane shock wave

Cites Work

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