1.
Design and Aerodynamic Performance Study of an S-shaped Inlet of the UAV;
一种无人机S弯进气道设计与气动特性研究
2.
Design and wind tunnel test of an axisymmetric inlet for ramjet engine
冲压发动机用轴对称进气道设计和试验
3.
Design of a two-dimensional mixed-compression supersonic inlet with boundary layer consideration
考虑附面层影响的二元混压式进气道设计
4.
The Mechanism of Bump Inlet and It's Design Laws
Bump进气道的机理与设计规律研究
5.
Research on the curvature parameter in the S-shaped inlet's stealth design
S弯进气道隐身设计中弯度参数研究
6.
Optimum Design of Inlet Air Core of Engine by CFD Technology
基于CFD的发动机进气道优化设计
7.
The Study on Design of Four-Valve Intake Port in 4V105 Diesel Engine;
4V105柴油机四气门缸盖进气道的设计研究
8.
Design and Experimental Verification of Hypersonic Inlet with Rectangular Section
矩形截面高超声速进气道气动设计及实验验证
9.
Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet;
高超声速进气道的设计、计算与实验研究
10.
Research and Optimize on Structure Parameters of Helical Intake Port for Diesel Engine;
柴油机螺旋进气道结构参数对气道性能的影响及其优化设计
11.
Design Modification and Model Selection on Ground Test for a Certain Aircraft Inlet
某飞机进气道改型方案的设计与地面选型试验
12.
Supersonic chin inlet/airframe integration design
超声速下颔式进气道/前机身一体化方案设计
13.
Design and Analysis of Placement Layers for Composite Laminates and Aircraft Inlet
复合材料层合板及飞机进气道铺层设计与分析
14.
Study of Optimization Method for Two-Dimensional Hypersonic Inlet
二维高超声速进气道优化设计方法研究
15.
Optimum design for 2-D inlet while large AOA considered
大攻角条件下的二维进气道型面优化设计
16.
Integrated design and performance research of waverider forebody/inlet
两种乘波前体/进气道一体化设计与性能研究
17.
A New Design Method for Diesel Helical Intake Port Parameter
一种新的柴油机螺旋进气道参数化设计方法
18.
On Optimization Design Genetic Algorithms of Two-dimensional Supersonic Inlet Based
基于遗传算法的超声速二维进气道优化设计