Unsteady hypersonic boundary layers for slender axisymmetric bodies with large injection rates
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Publication:1199177
DOI10.1016/0020-7225(92)90108-SzbMath0753.76085OpenAlexW2035807102MaRDI QIDQ1199177
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
skin frictionimplicit finite difference schemesemi-similar solutiontransverse curvatureaccelerating/decelerating streamfluctuating streamquasi- linearization technique
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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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