PEGASUS 5: An automated preprocessor for overset-grid computational fluid dynamics

被引:80
作者
Rogers, SE
Suhs, NE
Dietz, WE
机构
[1] NASA, Ames Res Ctr, Adv Supercomp Div, Moffett Field, CA 94035 USA
[2] USA, Aviat & Missile Command, Aviat Engn Directorate, Aeromech Div, Redstone Arsenal, AL 35898 USA
[3] Flow Anal Inc, Tullahoma, TN 37330 USA
关键词
D O I
10.2514/2.2070
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An all new, automated version of the PEGASUS software has been developed and tested. PEGASUS provides the hole-cutting and connectivity information between overlapping grids and is used as the final part of the grid-generation process for overset-grid computational fluid dynamics approaches. The new PEGASUS code (Version 5) has many new features: automated hole cutting, a projection scheme for fixing small discretization errors in overset surfaces, more efficient interpolation search methods using an alternating digital tree and a stencil-jumping scheme, hole-size optimization based on adding additional layers of fringe points, and an automatic restart capability. The new code has also been parallelized using the message-passing interface standard. The parallelization performance provides efficient speedup of the execution time by an order of magnitude, and up to a factor of 30 for very large problems. The results of two example cases are presented: a three-element high-lift airfoil and a complete Boeing 777-200 aircraft in a high-lift landing configuration. Comparisons of the computed flowfields for these test cases between the old and new versions of the PEGASUS codes show excellent agreement with each other and with experimental results.
引用
收藏
页码:1037 / 1045
页数:9
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