aeroacoustic

基本解釋

Inverse Aeroacoustic Problem for a Rectangular Wing.
長(zhǎng)方形翼逆航空聲學(xué)問(wèn)題。
The aeroacoustic field generated by a transonic two-blade Hartzell propeller was calculated by using Kirchhoff method.
本文采用Kirchhof方法計(jì)算雙槳葉Hartzel跨音速螺旋槳的遠(yuǎn)場(chǎng)氣動(dòng)噪聲。
It is very significant to obtain the aeroacoustic sources distribution around a vehicle effectively and efficiently.
快速有效的獲得車(chē)身周?chē)鷼鈩?dòng)噪聲源分布具有重要意義。
Furthermore, the resonator can reduced the aeroacoustic noise a little but decreased the flow rate.
不過(guò)由于加裝共振器，會(huì)使風(fēng)機(jī)之入風(fēng)口速度降低，因而減少其整體流量；
Aeroacoustic governing equations is established for non-concentric perforated mufflers based on one dimensional plane wave theory.
摘要根據(jù)管道一維平面波理論對(duì)非同軸穿孔消聲器，建立聲學(xué)控制方程。