A study of moderately underexpanded single and twinjet rocket exhaust plumes in quiescent and in a mach 7 hypersonic freestream

A study of moderately underexpanded single and twinjet rocket exhaust plumes in quiescent and in a mach 7 hypersonic freestream

Rocket plume flowfields have an importance due to their influence on the signature of the rocket and also on the distribution of the plume gases around the vehicle. Little information on the co-flowing situation exists other than a previous study at Oxford. This thesis thus represents a significant...

書誌詳細
主要な著者:	Shek, H, Shek, Howard
フォーマット:	学位論文
言語:	English
出版事項:	1997
主題:	Smoke plumes Aerodynamics, Hypersonic

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