DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION

He Zhongwei

Volume 3 Issue 3

Jul. 1988

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Article Navigation > Journal of Aerospace Power > 1988 > 3(3): 259-261,286

He Zhongwei. DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION[J]. Journal of Aerospace Power, 1988, 3(3): 259-261,286.

Citation:

He Zhongwei. DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION[J]. Journal of Aerospace Power, 1988, 3(3): 259-261,286.

He Zhongwei. DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION[J]. Journal of Aerospace Power, 1988, 3(3): 259-261,286.

Citation:

He Zhongwei. DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION[J]. Journal of Aerospace Power, 1988, 3(3): 259-261,286.

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DYNAMIC DISTORTION IN FLOWFIELD DOWNSTREAM OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION

He Zhongwei

Nanjing Aeronautical Institute

Received Date: 1987-11-01
Publish Date: 1988-07-28

Abstract

Abstract

The dynamic diatortions in flowfield under transonic shock-turbulent boundary layer interaction of different intensity are investigated in a 2-D convergent-divergent duct.The power spectrum and probability density functions of the total pressure signals are analyzed. The control technique of this dynamic distortion is also presented.