A Reactive, Equilibrium Hypersonic Flow Over a Slender Pointed Body

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概要

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• A reactive, equilibrium hypersonic gas flow over a slender body is treated. The reaction considered is υ_1A+υ_2B=(υ_1+υ_2)C, and it is assumed that the molecular weights ,and the specific heats at constant pressure of species "A", "B" and "C" are the same respectively. It is show that approximate similarity solutions exist for power law bodies r_b∼x^m. Numerical results for several values of m for two dimensional bodies and bodies of revolution are presented for the reaction N_2+O_2=2NO.

• 社団法人日本物理学会の論文
• 1971-02-05

著者

• Yasuhara Michiru

  Department of Mechanical Engineering, Aichi Institute of Technology

• Kondo Toshio

  Department Of Aeronautical Engineering Nagoya University

• Yasuhara Michiru

  Department Of Aeronautical Engineering Nagoya University

• YASUHARA Michiru

  Department of Aeronautical Engineering, Nagoya University

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• A Reactive, Equilibrium Hypersonic Flow Over a Slender Pointed Body
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• Flow of a Viscous, Electrically Conducting Fluid along a Circular Cylinder or a Flate Plate with Uniform Suction
• Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution

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