首页> 美国政府科技报告 >Development and Application of Computational Aerothermodynamics Flowfield Computer Codes. Terminal Progress Report, September 1, 1986-October 31, 1987
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Development and Application of Computational Aerothermodynamics Flowfield Computer Codes. Terminal Progress Report, September 1, 1986-October 31, 1987

机译:计算气动热力学流场计算机程序的开发与应用。终端进展报告,1986年9月1日至1987年10月31日

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摘要

Multiple nozzle plume flow field is computed with a 3-D, Navier-Stokes solver. Numerical simulation is performed with a flux-split, two-factor, time asymptotic viscous flow solver of Ying and Steger. The two factor splitting provides a stable 3-D solution procedure under ideal-gas assumptions. An ad-hoc acceleration procedure that shows promise in improving the convergence rate by a factor of three for steady state problems is utilized. Computed solutions to generic problems at various altitude and flight conditions show flow field complexity and three-dimensional effects due to multiple nozzle jet interactions. Viscous, ideal gas solutions for the symmetric nozzle are compared with other numerical solutions.

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