APPLICATION OF A MULTIBLOCK CFD CODE TO INVESTIGATE THE IMPACT OF GEOMETRY MODELING ON CENTRIFUGAL-COMPRESSOR FLOW-FIELD PREDICTIONS

Citation
Md. Hathaway et Jr. Wood, APPLICATION OF A MULTIBLOCK CFD CODE TO INVESTIGATE THE IMPACT OF GEOMETRY MODELING ON CENTRIFUGAL-COMPRESSOR FLOW-FIELD PREDICTIONS, Journal of turbomachinery, 119(4), 1997, pp. 820-830
Citations number
13
Categorie Soggetti
Engineering, Mechanical
Journal title
ISSN journal
0889504X
Volume
119
Issue
4
Year of publication
1997
Pages
820 - 830
Database
ISI
SICI code
0889-504X(1997)119:4<820:AOAMCC>2.0.ZU;2-5
Abstract
CFD codes capable of utilizing multi-block grids provide the capabilit y to analyze the complete geometry of centrifugal compressors includin g, among others, multiple splitter rows, tip clearance, blunt trailing edges, fillets, and slots between moving and stationary surfaces. Att endant with this increased capability is potentially increased grid se tup time and more computational overhead-CPU time and memory requireme nts-with the resultant increase in ''wall clock'' time to obtain a sol ution. If the increase in ''difficulty'' of obtaining a solution signi ficantly improves the solution from that obtained by modeling the feat ures of the tip clearance flow or the typical bluntness of a centrifug al compressor's trailing edge, then the additional burden is worthwhil e. However, if the additional information obtained is of marginal use, then modeling of certain features of the geometry may provide reasona ble solutions for designers to make comparative choices when pursuing a new design. In this spirit a sequence of grids were generated to stu dy the relative importance of modeling versus detailed gridding of the tip gap and blunt trailing edge regions of the NASA large low-speed c entrifugal compressor for which there is considerable detailed interna l laser anemometry data available for comparison. The results indicate : (I) There is no significant difference in predicted tip clearance ma ss flow rare whether the tip gap is gridded or modeled. (2) Gridding r ather than modeling the trailing edge results in better predictions of some flow details downstream of the impeller but otherwise appears to offer no great benefits. (3) The pitchwise variation of absolute flow angle decreases rapidly up to 8 percent impeller radius ratio and muc h more slowly thereafter. Although some improvements in prediction of flow field details are realized as a result of analyzing the actual ge ometry there is no clear consensus that any of the grids investigated produced superior results in every case when compared to the measureme nts. However, if a multi-block code is available, it should be used, a s it has the propensity for enabling better predictions than a single block code, which requires modeling of certain geometry features. If a single block code must be used, some guidance is offered for modeling those geometry features that cannot be directly gridded.