Title of article
Navier-Stokes Computation of Grid Fin Missile Using Hybrid Structured-Unstructured Grids
Author/Authors
DENG، نويسنده , , You-qi and MA، نويسنده , , Ming-sheng and ZHENG، نويسنده , , Ming and ZHOU، نويسنده , , Nai-chun، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2006
Pages
5
From page
304
To page
308
Abstract
Viscous CFD computations are performed to predict the aerodynamic coefficients and flowfield for a missile with grid fins by using hybrid structure-unstructured grids. The computations are made at Mach numbers of 0.7 and 2.0. Full N-S equations are discretized into finite volume form and solved by an algorithm in LU-SGS. The comparisons between computation and experimental data are made, and the detailed flow structure near grid fin is shown and examined.
Keywords
Steady flow , Navier-Stokes equation , hybrid structure-unstructured grid , Computational fluid dynamics , grid fin missile , finite volume
Journal title
Chinese Journal of Aeronautics
Serial Year
2006
Journal title
Chinese Journal of Aeronautics
Record number
2264597
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