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Combustion Generated Heat Addition to a Ducted Supersonic Stream. I. Theory

机译：燃烧产生的热量加入管道超音速流。一，理论

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作者
Isaac, J. J.; Cookson, R. A.;
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年度 1977
页码 p.1-22
总页数 22
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerothermodynamics; Supersonic combustion; Heat of combustion; Ignition; Gas dynamics; Mach number; Great Britain; Reprints;

机译：航空动力学;超音速燃烧;燃烧热;点火;气体动力学;马赫数;英国;重印;

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2. Erratum: On the One‐Dimensional Theory of Steady Compressible Fluid Flow in Ducts with Friction and Heat Addition [J] . Journal of Applied Physics . 1948,第6期

机译：勘误：关于带有摩擦和热量增加的管道中稳定可压缩流体流动的一维理论
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5. HEAT ADDITION TO A SUPERSONIC FLOW. [D] . BURSON, WILLIAM CLEAVER, JR. 1975

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6. An Examination of Dr. Crawfords Theory of Heat and Combustion [O] . 1781

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7. An analytical theory of heated duct flows in supersonic combustors [O] . Chenxi Wu, Fengquan Zhong, Jing Fan 2014

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8. Combustion Generated Heat Addition to a Ducted Supersonic Stream. II. Experimental Study [R] . Cookson, R. A., Isaac, J. J. 1977

机译：燃烧产生的热量加入管道超音速流。 II。实验研究

Combustion Generated Heat Addition to a Ducted Supersonic Stream. I. Theory

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