A Calculating Method of Shock Wave Oscillating Frequency Due to Turbulent Shear Layer Fluctuations in Supersonic Flow

Xu Li-gong; Ran Zheng

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Article Navigation > Applied Mathematics and Mechanics > 1991 > 12(8): 729-735

Xu Li-gong, Ran Zheng. A Calculating Method of Shock Wave Oscillating Frequency Due to Turbulent Shear Layer Fluctuations in Supersonic Flow[J]. Applied Mathematics and Mechanics, 1991, 12(8): 729-735.

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A Calculating Method of Shock Wave Oscillating Frequency Due to Turbulent Shear Layer Fluctuations in Supersonic Flow

Xu Li-gong¹,
Ran Zheng²

1.
Department of Modern Mechanics, University of Science and Technology of China, Hefei;
2.
Division of Postgraduate, China Aerodynamics Research and Development Center, Mianyang, Sichuan

Received Date: 1990-08-20
Publish Date: 1991-08-15

Abstract

Abstract

One of the more severe fluctuating pressure environments encountered in supersonic or hypersonic flows is the shock wave oscillation driven by interaction of a shock wave with boundary layer. The high intensity oscillating shock wave may induce structure resonance of a high speed vehicle. The research for the shock oscillation used to adopt empirical or semiempirical methods because the phenomenon is very complex. In this paper a theoretical solution on shock oscillating frequency due to turbulent shear layer fluctuations has been obtained from basic conservation equations. Moreover, we have attained the regularity of the frequency of oscillating shock varying with incoming flow Much numbers M_∞ and turning angle θ. The calculating results indicate excellent agreement with measurements. This paper has supplied a valuable analytical method to study aeroelastic problems produced by shock wave oscillation.
- shock wave oscillation,
- interaction of shock wave with boundary layer,
- fluctuating pressure,
- eigenfrequency of shock wave,
- turbulent acoustic radiation,
- aeroelastics

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References(8)

References

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