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Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe

机译：6马赫超音速输送机体对流冷却系统的设计

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摘要

Results of analytical and design studies are presented for a water-glycol convective cooling system for the airframe structure of a hypersonic transport. System configurations and weights are compared. The influences of system pressure drop and flow control schedules on system weight are defined. (Author)

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Helenbrook, R. G.; Anthony, F. M.;
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年度 1971
页码 p.1-131
总页数 131
原文格式 PDF
正文语种 eng
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关键词
Cooling systems ; Hypersonic aircraft ; Systems engineering ; Transport aircraft ; Airframes ; Aluminum alloys ; Convective heat transfer ; Glycols ; Mach number ; Mathematical models ; Thermodynamics;

机译：冷却系统;高超音速飞机;系统工程;运输机;机身;铝合金;对流传热;乙二醇;马赫数;数学模型;热力学;

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6. Effect of increased convective clearance by on-line hemodiafiltration on all cause and cardiovascular mortality in chronic hemodialysis patients – the Dutch CONvective TRAnsport STudy (CONTRAST): rationale and design of a randomised controlled trial ISRCTN38365125 [O] . E Lars Penne, Peter J Blankestijn, Michiel L Bots, 2005

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7. Design of a convective cooling system for a Mach 6 hypersonic transport airframe [O] . Anthony, F. M., Helenbrook, R. G. 1971

机译：Mach 6高超音速运输机体的对流冷却系统设计
8. Design of a convective cooling system for a Mach 6 hypersonic transport airframe [R] . Helenbrook, R. G., Anthony, F. M. 1971

机译：用于mach 6高超音速运输机体的对流冷却系统的设计

Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe

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