Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge.

Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge.

著者名:

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : GT

シリーズ巻号:

2005

発行年:

2005

通号:

GT2005-69003

ペーパー番号:

GT2005-69003

総ページ数:

12

出版情報:

New York, NY: 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:	ZA00001650
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2005
回次:	2005
会議開催地:	Reno-Tahoe, NV., USA
会議開催年:	2005.06.06-2005.06.09
論文注記:	ASME Turbo Expo 2005, Reno-Tahoe, NV., USA, June 6-9, 2005

類似資料:

1 テクニカルペーパー Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge. Mouzon, B.D., Albert, J.E., Terrell, E.J., Bogard, D.G. American Society of Mechanical Engineers	7 テクニカルペーパー Effect of coolant injection on heat transfer for a simulated turbine airfoil leading edge Yuki, Ushio M., Bogard, David G., Cutbirth, J. Michael The American Society of Mechanical Engineers
2 国際会議録 Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge Elon J. Terrell, Brian D. Mouzon, David G. Bogard American Society of Mechanical Engineers	8 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
3 国際会議録 Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge Brian D. Mouzon, Elon J. Terrell, Jason E. Albert, David G. Bogard American Society of Mechanical Engineers	9 テクニカルペーパー Leading edge film cooling effects on turbine blade heat transfer Garg, Vijay K., Gaugler, Raymond E. The American Society of Mechanical Engineers
4 テクニカルペーパー Effect of Regular and Random Roughness on the Heat Transfer and Skin Friction Coefficient on the Suction Side of a Gas Turbine Vane. Dees, J.E., Bogard, D.G. American Society of Mechanical Engineers	10 テクニカルペーパー Leading edge film cooling effects on turbine blade heat transfer Garg, Vijay K., Gaugler, Raymond E. National Aeronautics and Space Adminstration
5 テクニカルペーパー Heat Transfer Augmentation Downstream of Rows of Various Dimple Geometries on the Suction Side of a Gas Turbine Airfoil. Dees, J., Bogard, D.G., Bunker, R.S. American Society of Mechanical Engineers	11 テクニカルペーパー Influence of high mainstream turbulence on leading edge film cooling heat transfer: Effect of film hole row location Ou, S., Mehendale, A. B., Han, J. C. The American Society of Mechanical Engineers
6 テクニカルペーパー The Effects of Obstructions on Film Cooling Effectiveness on the Suction Side of a Gas Turbine Vane. Demling, P., Bogard, D.G. American Society of Mechanical Engineers	12 テクニカルペーパー High Resolution Film Cooling Effectiveness Comparison of Axial and Compound Angle Holes on the Suction Side of a Turbine Vane. Waye, S.K., Bogard, D.G. American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12