The present paper is aiming at describing the injectant behaviors from two rows of film cooling holes with opposite orientation angles. Boundary layer temperature distributions were measured in the streamwise normal plane to illustrate the interaction between the injectant from the holes in the upst
โฆ LIBER โฆ
Effectiveness of gas-film cooling in a circular tube with adiabatic walls
โ Scribed by T. F. Bekmuratov
- Publisher
- Springer US
- Year
- 1968
- Tongue
- English
- Weight
- 165 KB
- Volume
- 14
- Category
- Article
- ISSN
- 1573-871X
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