1.
Numerical Simulation of Effect of Inlet Total-Pressure Distortion on Subsonic Axial-Flow Compressor
进口总压畸变对亚声速轴流压气机流场影响数值研究
2.
Investigation of Compressor Stability with Distortion by Inlet Insert-board;
压气机进口插板总压畸变稳定性研究
3.
Numerical simulation of the inlet total temperature distortion in the compressor
进气总温畸变在压气机中的数值模拟
4.
Experimental study of inlet total-pressure distortion on four kinds of flat baffles
多种形式插板的压气机进气总压畸变实验
5.
The Inlet Total Pressure Distortion Index Forecast Based on RBF Neural Networks;
基于RBF神经网络发动机进气总压畸变指数预报
6.
The numerical simulation of the total pressure distortion in the inlet with flashboard
进气道插板式总压畸变试验的数值模拟
7.
Investigation of disturbed board total pressure distortion on a certain turbofan engine
某型涡扇发动机扰流板进气总压畸变研究
8.
Numerical simulation of the effect of total pressure inlet distortion on a compressor rotor
总压进气畸变对压气机转子气动影响的数值模拟
9.
Numerical simulation of full annuls of a transonic fan with distorted inlet
总压畸变对风扇流场影响的全流道数值研究
10.
Two-dimensional incompressible model of effects of rotating inlet distortion on flow instability in compression systems
旋转总压畸变对压气机稳定性影响的二维不可压缩模型
11.
All Annulus Numerical Simulation of Total Pressure Distortion Effect in a Transonic Fan;
总压畸变对跨声速风扇流场结构影响的全流道数值模拟
12.
Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow
畸变进气时涡扇发动机整机环境下压缩部件气动稳定性评定
13.
Investigations on Off-Design Performance Computation and Predicting Methods of Inlet Flow Distortion for Fan/Compressor;
风扇/压气机非设计点性能计算和进气畸变影响预测方法研究
14.
Test-based syntonic analysis of the aero-engine inserted-board inlet dynamic distortion pressure
基于实验的发动机插板式进气畸变压力谐振分析
15.
The Blowing-off of the Lip Separation of an Axisymmetric Supersonic Inlet and the Analysis of the Coherence of Dynamic Distortion of the Inlet
超音速轴对称进气道唇口分离流吹除及其动态畸变源相干分析
16.
An Improved CFD-synthesis Method for Predicting Inlet Dynamic Distortion
改进的综合CFD与畸变合成法预测动态畸变(英文)
17.
The air pressure at the hot value inlet does not become excessively low.
在热风阀进口处的风压不要变得太低。
18.
Influence of inlet dynamic total pressure flow field on gas-turbine engine stability margin
进口动态总压流场对燃机稳定性裕度影响