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PROJECT SQUID. An Evaluation of the Heat Transfer Encountered in a Rocket Motor Operating at High Chamber Pressures

机译：项目sQUID。在火箭发动机工作在遇到高的室压传热评价

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作者
Warner, C. F.; Zucrow, M. J.;
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年度 1949
页码 p.1-30
总页数 30
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Heat transfer; Combustion chambers; Rocket engines; Heat of combustion; Combustion chamber gases; Oxidation; Pressure; Jet propulsion;

机译：传热;燃烧室;火箭发动机;燃烧热;燃烧腔室的气体;氧化;压力;喷射推进;

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专利

1. NUMERICAL EVALUATION OF HEAT TRANSFER ENHANCEMENT IN ROCKET THRUST CHAMBERS BY WALL RIBS [J] . B. Betti, F. Nasuti, E. Martelli Numerical Heat Transfer, Part A. Application: An International Journal of Computation and Methodology . 2014,第1a6期

机译：壁肋对火箭推力箱传热强化的数值评估
2. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors [J] . Emelyanov V. N., Teterina I. V., Volkov K. N., Acta astronautica . 2017,第JUNa期

机译：固体火箭发动机燃烧室中的压力振荡和工作过程的不稳定性
3. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [J] . Marco Pizzarelli Data in Brief . 2021,第a期

机译：液体火箭发动机推力室喉部区域的实验测量热传递的数据集
4. Pressures encountered in the operating theater as a source of bacterial infection [C] . Altman, K.W., McElhaney, Engineering in Medicine and Biology Society, 1989. Images of the Twenty-First Century., Proceedings of the Annual International Conference of the IEEE Engineering in . 1989

机译：手术室遇到的压力是细菌感染的来源
5. INVESTIGATION OF COMBUSTION CHARACTERISTICS OF A HIGH CHAMBER PRESSURE ROCKET MOTOR. [D] . CARPENTER, THOMAS WILLIAM. 1969

机译：高腔压力火箭发动机燃烧特性的研究。
6. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [O] . Marco Pizzarelli 2021

机译：实验测量的热传递的数据集在液体火箭发动机推力室的喉部区域中的热传递
7. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors [O] . Emelyanov V.N., Teterina I.V., Volkov K.N., 2017

机译：固体火箭发动机燃烧室内的压力振荡和工作过程的不稳定性

PROJECT SQUID. An Evaluation of the Heat Transfer Encountered in a Rocket Motor Operating at High Chamber Pressures

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