| 单词 | nozzle thrust coefficient | 
| 释义 | nozzle thrust coefficient [`näz·ǝl ¦thrǝst ´kō·i´fish·ǝnt]  AEROSPACE ENGINEERING A measure of the amplification of thrust due to gas expansion in a particular nozzle as compared with the thrust that would be exerted if the chamber pressure acted only over the throat area. Also known as thrust coefficient.  | 
	
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