Unsteady hypersonic boundary layers for slender axisymmetric bodies with large injection rates

DOI10.1016/0020-7225(92)90108-SzbMath0753.76085OpenAlexW2035807102MaRDI QIDQ1199177

S. Roy, G. Nath

Publication date: 16 January 1993

Published in: International Journal of Engineering Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7225(92)90108-s

zbMATH Keywords

skin frictionimplicit finite difference schemesemi-similar solutiontransverse curvatureaccelerating/decelerating streamfluctuating streamquasi- linearization technique

Mathematics Subject Classification ID

Cites Work

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• Compressible boundary-layer flow at a three-dimensional stagnation point with massive blowing
• Finite-Difference Version of Quasi-Linearization Applied to Boundary-Layer Equations
• Fast and stable numerical method for boundary-layer flow with massive blowing
• Laminar flow at a three-dimensional stagnation point with large rates of injection
• Boundary-layer flows with large injection and heat transfer.
• Axisymmetric hypersonic flow with strong viscous interaction
• Unsteady laminar boundary layers on an infinite plate in an optically thick radiating gas
• On laminar boundary-layer blow-off. Part 2

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