Numerical Simulation of Supersonic Gap Flow

Abstract

Various gaps in the surface of the supersonic aircraft have a significant effect on airflows. In order to predict the effects of attack angle, Mach number and width-to-depth ratio of gap on the local aerodynamic heating environment of supersonic flow, two-dimensional compressible Navier-Stokes equations are solved by the finite volume method, where… (More)
DOI: 10.1371/journal.pone.0117012

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Cite this paper

@inproceedings{Jing2015NumericalSO, title={Numerical Simulation of Supersonic Gap Flow}, author={Xu Jing and Huang Haiming and Huang Sheng Guo and Mo Song}, booktitle={PloS one}, year={2015} }