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1.
A design method was developed to specify the profile of the continuously variable Mach-number nozzle for the supersonic wind tunnel. The controllable contour design technique was applied to obtaining the original nozzle profile, while other Machnumbers were derived from the transformation of the original profile. A design scheme, covering a Mach-number range of3.0相似文献
2.
根据等直径喷管内粉气流运动行为的数学模型以及实验研究，提出用实测初始运动参数确定喷管内粉粒初始速度的方法．并讨论了粉气比、粉粒初速和初始压强等参数之间的关系． 相似文献