Die inkompressible Grenzschicht höherer Ordnung am rotationssymmetrischen Staupunkt bei starkem Absaugen oder Ausblasen

DOI10.1007/BF01595199zbMath0282.76030MaRDI QIDQ1844127

N. R. Rajappa

Publication date: 1973

Published in: ZAMP. Zeitschrift für angewandte Mathematik und Physik (Search for Journal in Brave)

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10)

Related Items (2)

Compressible second-order boundary layers for three-dimensional stagnation point flows with mass transfer ⋮ Heat transfer in boundary layer flow of a micropolar fluid past a curved surface with suction and injection

Cites Work

• Unnamed Item
• The blowhard problem - inviscid flows with surface injection
• Mass-transfer effects on higher-order boundary layer solutions: The leading edge of a swept cylinder
• The asymptotic form of the laminar boundary-layer mass-transfer rate for large interfacial velocities
• Higher approximations in boundary-layer theory Part 1. General analysis
• The equation of similar profiles in boundary layer theory with strong blowing
• Higher approximations in boundary-layer theory Part 2. Application to leading edges
• Grenzen der Grenzschichtbeeinflussung

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