Study of Radiative Heat Transfer in Film Cooled LH/LO Rocket Engines Thrust Chamber.

Study of Radiative Heat Transfer in Film Cooled LH/LO Rocket Engines Thrust Chamber.

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2002

発行年:

2002

通号:

2002-0920

ペーパー番号:

2002-0920

総ページ数:

8

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001706
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	40th
会議開催地:	Reno, NV
会議開催年:	2002.01.14-2002.01.17
論文注記:	40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 14-17 January 2002

類似資料:

1 テクニカルペーパー Numerical Investigations of Geometric Design Parameters Defining Nozzle Guide Vane Endwall Heat Transfer. Rubensdorffer, F., Fransson, T.H. American Society of Mechanical Engineers	7 テクニカルペーパー Heat Transfer in Film-Cooled Bipropellant Thruster. Ohminami, K., Uesugi, K.T., Ogawa, H. Society of Automotive Engineers
2 テクニカルペーパー Heat Transfer Simulations in Liquid Rocket Engine Subscale Thrust Chambers H. Negishi, A. Kumakawa, N. Yamanishi, A. Kurosu American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Effect of a Blocked Channel on the Wall Temperature of a Regeneratively Cooled Rocket Thrust Chamber Naraghi,Mohammad H., Quentmeyer,Richard J., Mohr,David H. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー An Experimental Study on Heat Transfer in a Pre-Chamber Type Diesel Engine Harigaya,Y., Ohyagi,S., Tsuji,H. Society of Automotive Engineering, Inc.	9 テクニカルペーパー Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter H. Namkoung, P. Han, K. Lee, Y. Kim, C. Kim, Y. Yoon American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Hot film and liquid crystal transition measurements in a cascade at varying RE and TU Svensdotter, S., Fransson, T.H. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Experimental Study on the Heat Transfer in the Compound Cooling Passage. Li, L., Ding, S-T., Xu, G-Q., Tao, Z., Deng, H-W. American Society of Mechanical Engineers
5 テクニカルペーパー The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios Kacynski, Kenneth J., Hoffman, Joe D. National Aeronautics and Space Adminstration	11 テクニカルペーパー Experimental Assessment of Instantaneous Heat Transfer in the Combustion Chamber and Exhaust Manifold Walls of Air-Cooled Direct Injection Diesel Engine. Mavropoulos, G.C., Rakopoulos, C.D., Hountalas, D.T. Society of Automotive Engineers
6 テクニカルペーパー A numerical study of radiation effects in gas turbine combustion chambers Eklund, D.R., Badinand, T., Fransson, T. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Influence of a Gap for Film Cooling on Transient Flow Characteristics of Rocket Engine Nozzles. Takahashi, M., Tomita, T., Sakamoto, H., Tamura, H., Watanabe, Y. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12