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Aerodynamic and Thermodynamic Characteristics of Supersonic Ramjet Engine with Mach Number between 3 and 7. Part II. Calculation and Analysis of Thermodynamic Properties

机译：马赫数在3到7之间的超音速冲压发动机的气动和热力学特性。第二部分。热力学性质的计算与分析

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Chung-Hua, W.; Kao-Lien, L.; Chen-Kang, T.; Tien-Kuei, L.;
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年度 1980
页码 p.1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Supersonic combustion ramjet engines; Mathematical models; Thermodynamics; Thermodynamic properties; Aerodynamic characteristics; Jet aircraft;

机译：超音速燃烧冲压式喷气发动机;数学模型;热力学;热力学性质;空气动力学特性;喷气式飞机;

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Aerodynamic and Thermodynamic Characteristics of Supersonic Ramjet Engine with Mach Number between 3 and 7. Part II. Calculation and Analysis of Thermodynamic Properties

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