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Momentum and heat transfer in laminar boundary layer behind shock wave

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Abstract

Analytical and numerical solutions are established for momentum and energy laminar boundary layer induced by a shock wave. The results indicated that skin friction σ decreases with increasing in velocity ratio ξ (1≤ξ<6). For each specified ξ (1≤ξ <6), temperature w(t) increases with increasing of T w but decreases with T e, and for a range of t ε [1, ξ], w(t) decreases with the increasing of t. Thermal diffusion increases with increasing of u w but decreases with increasing u e.

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Authors and Affiliations

  1. Department of Mathematics & Mechanics, University of Science and Technology Beijing, 100083, Beijing, China

    Liancun Zheng

  2. Mechanical Engineering School, University of Science and Technology Beijing, 100083, Beijing, China

    Xinxin Zhang

  3. Thermal Engineering Department, Northeastern University, 110006, Shenyang, China

    Jicheng He

Authors
  1. Liancun Zheng
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  2. Xinxin Zhang
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  3. Jicheng He
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Zheng, L., Zhang, X. & He, J. Momentum and heat transfer in laminar boundary layer behind shock wave. J. of Therm. Sci. 11, 255–258 (2002). https://doi.org/10.1007/s11630-002-0063-8

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  • DOI: https://doi.org/10.1007/s11630-002-0063-8

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