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Numerical Simulation of the Tip Aerodynamics and Acoustics Test

F Tejero E P Doerffer O Szulc J L Cross

热科学学报（英文版）2016，Vol.25Issue(2)：153-160,8.

热科学学报（英文版）2016，Vol.25Issue(2)：153-160,8.DOI:10.1007/s11630-016-0846-y

Numerical Simulation of the Tip Aerodynamics and Acoustics Test

F Tejero E ¹P Doerffer ¹O Szulc ¹J L Cross²

作者信息

1. The Szwalski Institute of Fluid-Flow Machinery, Polish Academy of Sciences.Fiszera 14, 80-231, Gdansk, Poland
2. NASA Ames Research Center(retired), Moffett Field, CA, USA
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摘要

关键词

AH-1G/TAAT/helicopter rotor/forward flight/chimera overlapping grid

Key words

AH-1G/TAAT/helicopter rotor/forward flight/chimera overlapping grid

引用本文复制引用

F Tejero E,P Doerffer,O Szulc,J L Cross..Numerical Simulation of the Tip Aerodynamics and Acoustics Test[J].热科学学报（英文版）,2016,25(2):153-160,8.

基金项目

This work was supported by the 7th Framework Programme project IMESCON (PITN-GA-2010-264672) and in part by PL-Grid Infrastructure. （PITN-GA-2010-264672）

热科学学报（英文版）

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ISSN：1003-2169

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