“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.
随便看	permanent pump permanent set permanent-split capacitor motor permanent starch permanent stop permanent storage permanent teeth permanent thermocline permanent water permanent wave permanganate permanganic acid Permasyn motor permatron permeability permeability alloy permeability-block method permeability coefficient permeability number permeability profile permeability trap permeability tuning permeable bed permeable membrane permeameter

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