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赵桂林, 彭辉, 胡亮, 张绵纯. 超音速流动中侧向喷流干扰特性的实验研究[J]. 力学学报, 2004, 36(5): 577-582. DOI: 10.6052/0459-1879-2004-5-2004-003
引用本文: 赵桂林, 彭辉, 胡亮, 张绵纯. 超音速流动中侧向喷流干扰特性的实验研究[J]. 力学学报, 2004, 36(5): 577-582. DOI: 10.6052/0459-1879-2004-5-2004-003
Experimental investigations of lateral jet interactions in supersonic flows[J]. Chinese Journal of Theoretical and Applied Mechanics, 2004, 36(5): 577-582. DOI: 10.6052/0459-1879-2004-5-2004-003
Citation: Experimental investigations of lateral jet interactions in supersonic flows[J]. Chinese Journal of Theoretical and Applied Mechanics, 2004, 36(5): 577-582. DOI: 10.6052/0459-1879-2004-5-2004-003

超音速流动中侧向喷流干扰特性的实验研究

Experimental investigations of lateral jet interactions in supersonic flows

  • 摘要: 在超音速流动中,进行了侧向喷流干扰特性的实验研究,研究了喷流压力、攻角、迎风侧及背风侧喷流对侧向喷流干扰特性的影响. 结果表明,随喷流压力增大,喷流前的高压区向前扩展,喷流的包裹作用加强. 有攻角时,背风侧喷流前的高压区更大,喷流包裹作用的影响区域前移,喷流的控制效果更好,这一趋势随攻角的增大更加明显.

     

    Abstract: Experimental investigation of the lateral jet interaction have beenperformed in supersonic flows to study the effects of jet pressures, angleof attacks, leeward side jet or windward side jet on the jet interactioncharacteristics. The results indicated that with increasing of jetpressures, the high pressure region before lateral jet extended forward, andthe wraparound effect strengthened. In the case of angle of attacks, thehigh pressure region before the leeward side jet enlarged, the region of jetwraparound effect moving forward, and the jet interaction control was moreeffective.

     

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