Compressible laminar boundary layer close to the leading edge of a swept wing in the presence of heat transfer and suction

DOI10.1007/BF01017413zbMath0319.76052MaRDI QIDQ1223007

A. N. Savoscik, A. D. Tohunc

Publication date: 1976

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

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• A new treatment of the lifting-line wing theory, with applications to rigid and elastic wings

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