The problem of minimizing the convective heat flux, transmitted from the boundary layer to the surface of a body in a flow, is considered under supersonic flow conditions. The specific coolant flow rate across a porous or perforated shell is regarded as the control, and the power of the cooling syst
โฆ LIBER โฆ
Vectored injection into compressible laminar and turbulent boundary layers
โ Scribed by D. Degani; M.Y. Hussaini; A.A. Wray
- Publisher
- Elsevier Science
- Year
- 1981
- Tongue
- English
- Weight
- 564 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0045-7825
No coin nor oath required. For personal study only.
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