1.
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
2.
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
3.
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
4.
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
5.
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
6.
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
7.
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
8.
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
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.
Design and Verification of Synthetical Pressure Distortion Index Calculation Software
综合压力畸变指数的计算软件设计及验证
12.
Simulation on the Response of A Single-stage Compressor to the Inlet Combined Distortion of Pressure and Temperature
某单级压气机对组合畸变响应特性的数值模拟
13.
Numerical Simulation Study of a Three-dimensional Unsteady Flow in a Fan Under Distorted Air Admission Conditions
畸变进气条件下风扇三维非定常流动数值模拟
14.
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
15.
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
16.
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
17.
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
18.
Numerical simulations of curved surface sidewall compression scramjet inlets with varied sweep angle and sidewall compression angle
变后掠角+变侧压角曲面压缩的高超侧压式进气道数值仿真