An innovative thermal management system for a Mach 4 to Mach 8 hypersonic scramjet engine

An innovative thermal management system for a Mach 4 to Mach 8 hypersonic scramjet engine

著者名:

Chen, Felix F. ( GenCorp-Aerojet )
Tam, William F. ( GenCorp-Aerojet )
Shimp, Nancy R. ( GenCorp-Aerojet )
Norris, Richard B. ( Air Force Research Laboratory )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

1998

発行年:

1998

通号:

98-3734

ペーパー番号:

98-3734

開始ページ:

1

終了ページ:

9

総ページ数:

9

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:	ZA00050858
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	34th
会議開催地:	Cleveland, OH
会議開催年:	1998.07.13-1998.07.15
論文注記:	34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 12-15, 1998/Cleveland, OH

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