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Hypersonic missiles- some problem areas

机译：高超音速导弹-一些问题领域

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摘要

An overview of some of the problems, which have to be overcome in the design of hypersonic missiles or projectiles, is given. In the main, these are connected with the high levels of heat transfer rate suffered by such vehicles, particularly those induced by aerodynamic control surfaces. Some of the aspects of heat transfer, induced by, and suffered by such controls are presented. Data are presented and discussed, regarding the effects of flow separation due to flaps or flares, the effects of sharp and bluff fins (both swept and unswept). Finally, the aerodynamic interactions and heat transfer rates induced by reaction control jets are presented.
机译：概述了高超声速导弹或弹丸设计中必须克服的一些问题。基本上，这些与此类车辆，尤其是由空气动力学控制面引起的车辆所遭受的高水平的传热率有关。介绍了由此类控制引起的热传递的某些方面。呈现和讨论了有关由于襟翼或火炬引起的流动分离的影响，尖锐和钝鳍（扫掠和未扫掠）的影响的数据。最后，介绍了反应控制射流引起的空气动力学相互作用和传热速率。

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