Abstract
An experimental study of the effectiveness of film cooling following secondary air injection through a porous section into a turbulent free stream is presented. Boundary-layer velocity and temperature profiles are described. The adiabatic wall temperatures are presented in terms of the film-cooling effectiveness. The effects of varying the secondary air temperature, the blowing rate, and the free-stream velocity are studied. It is found that the protection given to a surface downstream of a porous section through which air is injected compares favorably to earlier studies where the secondary air was injected nearly tangential to the surface.
Dates
Type | When |
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Created | 13 years, 5 months ago (Feb. 28, 2012, 8:21 a.m.) |
Deposited | 5 years, 10 months ago (Oct. 5, 2019, 2:29 a.m.) |
Indexed | 1 year, 8 months ago (Dec. 4, 2023, 6:17 a.m.) |
Issued | 60 years ago (Aug. 1, 1965) |
Published | 60 years ago (Aug. 1, 1965) |
Published Online | 60 years ago (Aug. 1, 1965) |
Published Print | 60 years ago (Aug. 1, 1965) |
@article{Goldstein_1965, title={Film-Cooling Effectiveness With Injection Through a Porous Section}, volume={87}, ISSN={1528-8943}, url={http://dx.doi.org/10.1115/1.3689114}, DOI={10.1115/1.3689114}, number={3}, journal={Journal of Heat Transfer}, publisher={ASME International}, author={Goldstein, R. J. and Shavit, G. and Chen, T. S.}, year={1965}, month=aug, pages={353–359} }