Turbine Nozzle Endwall Inlet Film Cooling- The Effect of a Back- Facing Step.

Turbine Nozzle Endwall Inlet Film Cooling- The Effect of a Back- Facing Step.

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:

2003

発行年:

2003

通号:

GT2003-38319

ペーパー番号:

GT2003-38319

総ページ数:

9

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:	ZA00001749
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2003
回次:	2003
会議開催地:	Atlanta, Georgia, USA
会議開催年:	2003.06.16-2003.06.19
論文注記:	ASME Turbo Expo 2003, Atlanta, Georgia, USA, 16-19 June 2003

類似資料:

1 テクニカルペーパー The Effect of Wall Thickness on Nozzle Suction Side Film Cooling. Zhang, L., Moon, H.K. American Society of Mechanical Engineers	7 テクニカルペーパー Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors: Near Wall Reaction Effects on Film-Cooled Backward-Facing Step Heat Transfer. Milanes, D. W., Kirk, D. R., Fidknowski, K. J., Waitz, I. A. American Society of Mechanical Engineers
2 テクニカルペーパー Turbine Blade Film Cooling Study: The Effects of Showerhead Geometry. Zhang, L., Moon, H.K. American Society of Mechanical Engineers	8 テクニカルペーパー Cooling effectiveness measurements with thermal radiometry in a turbine cascade Moon, H. K., Jaiswal, R. American Society of Mechanical Engineers
3 テクニカルペーパー Application of advanced experimental techniques in the development of a cooled turbine nozzle Moon, H.K., Glezer, B. The American Society of Mechanical Engineers	9 テクニカルペーパー A New Test Rig for Film Cooling Experiments on Turbine Endwalls. Kunze, M., Preibisch, S., Vogeler, K., Landis, K., Heselhaus, A. American Society of Mechanical Engineers
4 テクニカルペーパー Turbine Blade Film Cooling Study: The Effects of Film Hole Location on the Pressure Side. Zhang, L., Moon, H-K. American Society of Mechanical Engineers	10 テクニカルペーパー Film cooling of the gas turbine endwall by discrete-hole injection Jabbari, M. Y., Marston, K. C., Eckert, E. R. G., Goldstein, R. J. The American Society of Mechanical Engineers
5 テクニカルペーパー Turbine Nozzle Endwall Film Cooling Study Using Pressure Sensitive Paint. Zhang, L.J., Jaiswal, R.S. American Society of Mechanical Engineers	11 テクニカルペーパー Computational Predictions of Endwall Film Cooling for a Turbine Nozzle Vane with an Asymmetric Contoured Passage. Okita, Y., Nakamata, C. American Society of Mechanical Engineers
6 テクニカルペーパー Application of a heat flux/calorimeter-based method to assess the effect of turbulence on turbine airfoil heat transfer Glezer, B., Moon, H. K., Zhang, L., Camci, C. The American Society of Mechanical Engineers	12 テクニカルペーパー Development of a wide range temperature pyrometer for gas turbine application Moon, H.K., Glezer, B., Mink, B., Marvin, W. The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12