Numerical Simulation of External-Compression Supersonic Inlet Flow Fields

Ping Wang (), Hong-wei Wang, Si-dong Wei, Xue-shan Liu, Qing-guo Zhang and Xin Hua
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Ping Wang: Aviation University of Air Force
Hong-wei Wang: Aviation University of Air Force
Si-dong Wei: Aviation University of Air Force
Xue-shan Liu: Aviation University of Air Force
Qing-guo Zhang: Aviation University of Air Force
Xin Hua: Aviation University of Air Force

Chapter Chapter 125 in The 19th International Conference on Industrial Engineering and Engineering Management, 2013, pp 1187-1193 from Springer

Abstract: Abstract In this paper, Method of CFD is used to simulate 2D flow fields for a certain external-compression supersonic inlet. It describes the methods of mesh generation, boundary conditions determination, convergence techniques of governing equation, and analyzes simulation result. The numerical results match well with the theory.

Keywords: Convergence; Flow fields; Numerical simulation; Supersonic inlet (search for similar items in EconPapers)
Date: 2013
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-38391-5_125

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DOI: 10.1007/978-3-642-38391-5_125

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