Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge

Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge

著者名:

掲載資料名:

ASME Turbo Expo 2005: Power for Land, Sea, and Air (GT2005)

シリーズ名:

ASME Symposia Volumes

シリーズ巻号:

TURBO EXPO 2005(3A)

発行年:

2005

巻:

3A

ペーパー番号:

GT2005-69002

開始ページ:

825

終了ページ:

832

総ページ数:

8

出版情報:

New York: American Society of Mechanical Engineers

ISBN:

9780791847268 [0791847268]

言語:

英語

請求記号:

A11661/2005

資料種別:

国際会議録

詳細

TDL書誌ID:	ZA00048722
シリーズID:	PA00000270
会議名:	ASME Turbo Expo
回次:	2005
会議開催地:	Reno-Tahoe, Nevada USA
会議開催年:	2005.06.06-2005.06.09

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 Turbine Airfoil Net Heat Flux Reduction with Cylindrical Holes Embedded in a Transverse Trench. Harrison, K.L., Dorrington, J.R., Bogard, D.G. American Society of Mechanical Engineers
3 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	9 国際会議録 Heat Transfer Augmentation Downstream of Rows of Various Dimple Geometries on the Suction Side of a Gas Turbine Airfoil Jason E. Dees, David G. Bogard, Ronald S. Bunker American Society of Mechanical Engineers
4 国際会議録 Turbine Airfoil Net Heat Flux Reduction With Cylindrical Holes Embedded in a Transverse Trench Katharine L. Harrison, John R. Dorrington, David G. Bogard, Ronald S. Bunker, Jason E. Dees American Society of Mechanical Engineers	10 国際会議録 The Effects of Obstructions on Film Cooling Effectiveness on the Suction Side of a Gas Turbine Vane Patricia Demling, David G. Bogard American Society of Mechanical Engineers
5 テクニカルペーパー Adibatic and Overall Effectiveness for a Film Cooled Blade. Albert, J. E., Bogard, D. G., Cunha, F. American Society of Mechanical Engineers	11 国際会議録 Influence of Blade Leading Edge Geometry on Turbine Endwall Heat(Mass) Transfer S. Han, R. J. Goldstein American Society of Mechanical Engineers
6 国際会議録 Effects of Regular and Random Roughness on the Heat Transfer and Skin Friction Coefficient on the Suction Side of a Gas Turbine Vane Jason E. Dees, David G. Bogard American Society of Mechanical Engineers	12 国際会議録 High Resolution Film Cooling Effectiveness Comparison of Axial and Compound Angle Holes on the Suction Side of a Turbine Vane Scot K. Waye, David G. Bogard American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12