Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies

DOI10.1017/S0022112064001422zbMath0158.23401MaRDI QIDQ5541242

R. T. Davis, Irmgard Flügge-Lotz

Publication date: 1964

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

fluid mechanics

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Cites Work

• The laminar compressible boundary-layer in the stagnation-point region of an axisymmetric blunt body including the second-order effect of vorticity interaction
• Boundary Layer Over a Flat Plate in Presence of Shear Flow
• Shock Wave and Flow Field Development in Hypersonic Re-Entry