Analysis of interactions between shock waves and laminar boundary layer with heat transfer
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Publication:1113758
DOI10.1007/BF01177041zbMath0661.76061OpenAlexW1997864826MaRDI QIDQ1113758
Publication date: 1988
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf01177041
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Cites Work
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions
- Compressible boundary layer and its low-speed equivalent.
- Self-induced separation
- On boundary layers and upstream influence. I. A comparison between subsonic and supersonic flows
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