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Some factors influencing heat transfer to liquid-propellant rocket-thrust-chamber coolant channels

机译：影响液体推进剂火箭 - 推力室冷却剂通道传热的一些因素

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摘要

Wall temperature and heat transfer patterns in liquid-propellant rocket thrust chamber coolant channels

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作者
Curren, A. N.; Krueger, R. C.;
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年度 1966
页码 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
COOLANTS; COOLING SYSTEMS; HEAT TRANSFER; LIQUID PROPELLANT ROCKET ENGINES; LIQUID ROCKET PROPELLANTS; ROCKET THRUST; THRUST CHAMBERS; WALL TEMPERATURE; COOLING SYSTEM; HEAT TRANSFER; LIQUID PROPELLANT ROCKET ENGINE;

机译：冷却液;冷却系统;传播热量;液体推进剂火箭发动机;液体火箭推进剂;火箭推力;推力室;壁温;冷却系统;传播热量;液体推进剂火箭发动机;

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Some factors influencing heat transfer to liquid-propellant rocket-thrust-chamber coolant channels

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