aeroacoustic

基本解釋

Inverse Aeroacoustic Problem for a Rectangular Wing.
長方形翼逆航空聲學問題。
The aeroacoustic field generated by a transonic two-blade Hartzell propeller was calculated by using Kirchhoff method.
本文采用Kirchhof方法計算雙槳葉Hartzel跨音速螺旋槳的遠場氣動噪聲。
It is very significant to obtain the aeroacoustic sources distribution around a vehicle effectively and efficiently.
快速有效的獲得車身周圍氣動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.
不過由于加裝共振器，會使風機之入風口速度降低，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.
摘要根據管道一維平面波理論對非同軸穿孔消聲器，建立聲學控制方程。