LACE for Rocket-Based Combined-Cycle

LACE for Rocket-Based Combined-Cycle

著者名:

Oike, M. ( Tohoku University, Institute of Fluid Science )
Kamijo, K.
Tanaka, D.
Yamada, H.
Yoshida, H.

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:

1999

発行年:

1999

通号:

99-0091

ペーパー番号:

99-0091

開始ページ:

1

終了ページ:

6

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:	ZA00050873
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	37th
会議開催地:	Reno, NV
会議開催年:	1999.01.11-1999.01.14
論文注記:	37th AIAA Aerospace Sciences Meeting and Exhibit January 11-14, 1999 / Reno, NV

類似資料:

1 テクニカルペーパー LACE for rocket-based combined-cycle Oike, M., Kamijo, K., Tanaka, D., Yamada, H., Yoshida, H. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Mode Transition Study of Turbine-Based Combined Cycle Engine Concepts M. Chen, Z. Zhu, H. Tang, D. Zhu, J. Zhang American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Preliminary Evaluation of Heat Exchanger for LACE Oike, M., Tanaka, D., Kamijo, K., Yamada, H., Yoshida, H. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A Combined Experimental/Computational Investigation of a Rocket Based Combined Cycle Inlet Smart,Michael K., Trexler,Carl A., Goldman,Allen L. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Rotor vibrations of turbopump due to cavitating flows in inducer Yoshida, M., Komatsu, T., Oike, M., Kamijo, K., Yamada, H. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Rocket based combined cycle nozzle analysis using NPARC Steffen, C.J., Jr., Smith, T.D., Yungster, S., Keller, D.J. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Experimental study on rotating cavitation of rocket propellant pump inducers Hashimoto, T., Yoshida, M., Watanabe, M., Kamijo, K., Tsujimoto, Y. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Performance of a Rocket-Ramjet Combined-Cycle Engine Model in Ejector Mode Operation S. Tomioka, M. Takegoshi, K. Kudo, K. Kato, S. Hasegawa,, K. Kobayashi American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Improvements of Inducer Inlet Backflow Characteristics Using 3-D Inverse Design Method. Ashihara, K., Goto, A., Kamijo, K., Yamada, H., Uchiumi, M. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Verification of Low NOx Performance of Simple Primary Rich Combustion Approach by a Newly Established Full Annular Combustor Test Facility. Makida, M., Yamada, H., Shimodaira, K., Yoshida, S., Kurosawa, Y. American Society of Mechanical Engineers
6 テクニカルペーパー Simultaneous Measurements of Aromatic Hydrocarbons in Exhaust using a Laser Ionization Method. Yamada, H., Misawa, K., Fujii, M., Tanaka, K., Suzuki, D. Society of Automotive Engineers	12 テクニカルペーパー Fatigue Strength of Rocket Pump Inducers M. Uchiumi, K. Kamijo, N. Sakazume, R. Mihara American Institute of Aeronautics and Astronautics

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