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Validation of High-Fidelity CFD/CAA Framework for Launch Vehicle Acoustic Environment Simulation Against Scale Model Test Data.

机译：验证用于运载火箭声学环境仿真的高保真CFD / Caa框架对比例模型试验数据。

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作者
Liever, P. A.; West, J. S.; Harris, R. E.;
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年度 2016
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
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关键词
Launch vehicles; Liftoff (launching); Acoustic properties; Computational fluid dynamics; Computational aeroacoustics; Acoustic simulation; Scale models; Galerkin method; Runge-kutta method; Computational grids;

机译：运载火箭;升空（发射）;声学特性;计算流体动力学;计算气动声学;声学模拟;比例模型; Galerkin方法; Runge-kutta方法;计算网格;

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3. Fluid Dynamic and Acoustic Optimization Methodology of a Motorbike Intake Airbox Using Multilevel Numerical CFD Models and Experimental Validation Tests [J] . Gianluca Montenegro, Augusto Della Torre, Tarcisio Cerri, SAE International Journal of Engines . 2013,第3期

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4. A High-Fidelity CFD/BEM Methodology For Launch Pad Acoustic Environment Prediction [C] . Abhijit Tosh, Peter Liever, Fritz Owens, AIAA aeroacoustics conference;AIAA/CEAS aeroacoustics conference . 2012

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8. Validation of High-Fidelity CFD/CAA Framework for Launch Vehicle Acoustic Environment Simulation against Scale Model Test Data. [R] . Liever, P. A., West, J. S., Harris, R. E. 2016

机译：验证用于比例模型试验数据的运载火箭声环境仿真的高保真CFD / Caa框架。

Validation of High-Fidelity CFD/CAA Framework for Launch Vehicle Acoustic Environment Simulation Against Scale Model Test Data.

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