Influence of high mainstream turbulence on leading edge film cooling heat transfer: Effect of film hole row location

Influence of high mainstream turbulence on leading edge film cooling heat transfer: Effect of film hole row location

著者名:

Ou, S. ( Texas A&M University )
Mehendale, A. B.
Han, J. C.

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : WA/HT

シリーズ巻号:

1990

発行年:

1990

通号:

90-WA/HT-5

ペーパー番号:

90-WA/HT-5

出版情報:

New York, NY: The American Society of Mechanical Engineers

言語:

英語

請求記号:

A11800

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00002344
シリーズID:	PA00000203
会議名:	Winter Annual Meeting
回次:	1990
会議開催地:	Dallas, Texas
会議開催年:	1990.11.25-1990.11.30
論文注記:	Presented at the Winter Annual Meeting Dallas, Texas - November 25-30, 1990

類似資料:

1 テクニカルペーパー Influence of mainstream turbulence on leading edge film cooling heat transfer through two rows of inclined film slots Ou, S., Han, J. C. The American Society of Mechanical Engineers	7 テクニカルペーパー Influence of Blade Leading Edge Geometry on Turbine Endwall Heat(Mass) Transfer. Han, S., Goldstein, R.J. American Society of Mechanical Engineers
2 テクニカルペーパー Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade with Two Rows Holes in a 1-1/2 Turbine Stage at Design and Off … Yang, H., Chen, H-C., Han, J-C., Moon, H-K. American Society of Mechanical Engineers	8 テクニカルペーパー Influence of Compound Angle on Adiabatic Film Cooling Effectiveness and Heat Transfer Coefficient for a Row of Shaped Film Cooling Holes. Brauckmann, D., Von Wolfersdort, J. American Society of Mechanical Engineers
3 テクニカルペーパー Unsteady wake over a linear turbine blade cascade with air and CO2 film injection: Part I - Effect on heat transfer coefficients Ou, Shichuan, Han, Je-Chin, Mehendale, Anant B., Lee, C. Pang The American Society of Mechanical Engineers	9 テクニカルペーパー Transient liquid crystal measurement of leading edge film cooling effectiveness and heat transfer with high free stream turbulence Ou, Shichuaan, Rivir, Richard, Meininger, Matthew, Soechting, Fred, Tabbita, Martin American Society of Mechanical Engineers
4 テクニカルペーパー Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge. Terrell, E.J., Mouzon, B.D., Bogard, D.G. American Society of Mechanical Engineers	10 テクニカルペーパー Small diameter film cooling hole heat transfer: The influence of the hole length Andrews, G. E., Bazdidi-Tehrani, F., Hussain, C. I., Pearson, J. P. The American Society of Mechanical Engineers
5 テクニカルペーパー Unsteady wake over a linear turbine blade cascade with air and CO2 film injection: Part II: Effect on film effectiveness and heat transfer distributions Mehendale, Anant B., Han, Je-Chin, Ou, Shichuan, Pang Lee, C. The American Society of Mechanical Engineers	11 テクニカルペーパー Effect of film-cooling hole location on turbulator heat transfer enhancement in turbine blade internal air-cooling circuits McDonough, J. M., Garzon, V. E., Schulte, D. E. The American Society of Mechanical Engineers
6 テクニカルペーパー Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels with Angled Ribs Under High Rotation Numbers. Liu, Y-H., Huh, M., Rhee, D-H., Han, J-C., Moon, H-K. American Society of Mechanical Engineers	12 テクニカルペーパー Heat Transfer in Trailing Edge, Wedge-Shaped Cooling Channels Under High Numbers. Wright, L.M., Liu, Y-H., Han, J-C., Chopra, S. American Society of Mechanical Engineers

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