Asymptotic solution to the problem of hypersonic flow over bodies in the neighborhood of the separation point of a thin shock layer

DOI10.1007/BF01090703zbMath0539.76061OpenAlexW2063293029MaRDI QIDQ794522

E. R. Abramovskij, N. N. Lychagin

Publication date: 1982

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

Full work available at URL: https://doi.org/10.1007/bf01090703

zbMATH Keywords

equation of motionconvex bodycontinuity equationseparation pointthree-dimensionalsuccessive approximationtwo-dimensionalshock layermatched expansionsinviscid perfect gasMach number tending to infinityNewton-Busemann formulanormal shockspecific heat ratio tending to onetypes of tip shapes

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

• Unnamed Item
• Unnamed Item
• Hypersonic flow past an airfoil with a Mach system of shock waves
• On a singular point in the Newtonian theory of hypersonic flow
• The separation of Newtonian shock layers
• Die Singularitätsstelle in der Grenzschichtmethode der Hyperschallgasdynamik