Investigations on the Flow Fields of Hypersonic Flow Past the Wall-Mounted Square Cylinder with Various Heights

Combined with the large eddy simulation (LES), a 3rd-order WENO scheme and the adaptive mesh refinement (AMR) technique, the hypersonic compressible flow (Ma=5) past wall-mounted square cylinders with different heights is simulated numerically. Our results reveal that with the variation of cylinder...

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Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2013, Vol.56(4), pp.223-228
Hauptverfasser:	XUE, Dawen, CHEN, Zhihua, JIANG, Xiaohai
Format:	Artikel
Sprache:	eng
Schlagworte:	Aeronautics Computer simulation Cylinders Finite element method Flow Separation Hypersonic Flow Large eddy simulation Mathematical analysis Pressure distribution Shock Wave Square Cylinder Vortex
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