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基于FW-H方程的旋翼气动声学计算研究 被引量:33

Aeroacoustic Calculation for Helicopter Rotor in Hover and in Forward Flight Based on FW-H Equation
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摘要 由流体力学N S方程导出的非齐次波动方程———FfowcsWilliams Hawkings方程(简称FW H方程),可以精确地描述在静止流体中运动的物体与流体相互作用的发声问题。以FW H方程为理论模型,将旋翼桨叶运动发声问题等效为包含桨叶的任意运动控制面(声源面)的声辐射问题,并在旋翼绕流Euler方程数值模拟的基础上,在时域内计算了悬停旋翼和前飞旋翼的声场。应用于UH 1H和AH 1/OLS两种旋翼模型的气动声学计算表明:计算结果与噪声实验值符合良好;所研制的程序不仅能够较准确地计算单极子噪声和偶极子噪声,而且具有较强的跨音速四极子噪声预测能力。 The Ffowcs Williams/Hawkings (FW-H) equation, which is directly derived from Navier-Stokes equations, has been the theoretical background of predicting the noise generated by moving bodies. For predicting the rotor noise, in the conventional solution of FW-H equation, the blade is utilized as the integration surface, and the complication is caused when calculating the quadrupole noise. In the present work, a form of FW-H equation applied for a permeable surface was employed for predicting the quadrupole noise aerodynamically generated by rotor both in hover and forward flight. Section 1 discusses the CFD calculation performed by solving the 3-D unsteady Euler's equations. Section 2 describes in detail the solution of the permeable-surface FW-H equation in the time domain. The computed results for all cases were compared with experimental data and a reasonable agreement has been achieved. It is also shown that the developed code is efficient and is capable of capturing the nonlinear quadrupole noise for transonic rotor.
出处 《航空学报》 EI CAS CSCD 北大核心 2003年第5期400-404,共5页 Acta Aeronautica et Astronautica Sinica
基金 国防科技重点实验室基金(51463020103HK003) 西北工业大学研究生创业种子基金(Z20030012)资助项目
关键词 旋翼 气动声学 FW—H方程 非定常欧拉方程 Acoustics Aerodynamics Calculations Computer simulation
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参考文献7

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