“nozzle thrust coefficient”的概念、定义、翻译、参考文献-科学参考

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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