Analysis of the three-dimensional turbulent boundary layer on the surface of an arbitrary body at large angles of attack
Three-dimensional compressible gas flow past an arbitrary model body at large angles of attack is analyzed in the framework of the boundary layer theory with allowance for heat transfer. The equations of a three-dimensional turbulent boundary layer are solved using computer codes, the data on the external inviscid flow, and the body geometry.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 213061
- Journal Information:
- Fluid Dynamics, Journal Name: Fluid Dynamics Journal Issue: 3 Vol. 30; ISSN 0015-4628; ISSN FLDYAH
- Country of Publication:
- United States
- Language:
- English
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