目前, 机体气动噪声的研究方法分成实验和数值预测两大部分, 实验包含飞行实验和风洞试验;
而数值预测包含有纯理论方法, 半经验方法, 纯数值方法, CFD 与" 声类比" 相结合的方法 …

Both aerodynamic and aeroacoustic measurements in wind tunnels are necessary for the
study of high-lift devices. The existing wind tunnels have difficulties in simultaneously …

This paper introduces the continuous wavelet transform method to analyze different multiple
tonal phenomena of the high-lift configurations, aiming at revealing the time-frequency …

Unsteady and massively separated flows past the rudimentary landing gear are investigated
using delayed detached-eddy-simulation and improved delayed detached-eddy-simulation …

AERODYNAMIC performance measurements, such as lift and drag measurements for
instance, are usually carried out in closed-section wind tunnels while acoustic tests are …

Two types of aeroacoustic wind-tunnel test section configurations have been tested in the
NASA Langley Quiet Flow Facility. The first is a more traditional open-jet configuration …

WITH the increasing requirements for airworthiness and economy of aircraft, aircraft noise
has been a major concern to people and needs more attention. In the last 40 years, engine …

The last 10 years have seen the establishment of the hybrid anechoic wind tunnel as a
significant tool for experimental aeroacoustics research. The hybrid anechoic wind tunnel …

This Paper describes a new method of correcting the wind tunnel wall interference of
permeable Kevlar test section walls. The classical three-dimensional panel method is …

In regard to aircraft noise mitigation, this paper focuses on noise emission by a simplified
nose landing gear (NLG), whose noise sources are identified by the means of sensor array …