An experimental and computational study leading to new test capabilities for the HYPULSE facility with a detonation driver

An experimental and computational study leading to new test capabilities for the HYPULSE facility with a detonation driver

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Advanced Measurement and Ground Testing Technology Conference

シリーズ巻号:

1996

発行年:

1996

通号:

96-2193

ペーパー番号:

96-2193

開始ページ:

1

終了ページ:

10

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:	ZA00050834
シリーズID:	PA00000145
会議名:	AIAA Advanced Measurement and Ground Testing Technology Conference
回次:	19th
会議開催地:	New Orleans, LA
会議開催年:	1996.06.17-1996.06.20
論文注記:	19th AIAA Advanced Measurement and Ground Testing Technology Conference, June 17-20, 1996/New Orleans, LA

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1 テクニカルペーパー Design, calibration and analysis of a tunnel mode of operation for the HYPULSE facility Bakos, R.J., Calleja, J.F., Erdos, J.I., Auslender, A.H., Sussman, M.A., Wilson, G.J. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー An Experimental and Computational Study of Pulsed Detonations in a Single Tube. Shimo, M., Meyer, S.E., Heister, S.D., Weng, C.S., Ji, J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Expansion of the scramjet ground test envelope of the HYPULSE facility Bakos, R.J., Castrogiovanni, A., Calleja, J.F., Nucci, L., Erdos, J.I. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー NUMERICAL STUDIES OF A DETONATION ANALOGUE Clarke, J.F. National Aeronautics and Space Administration
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