1.
A Study of New Type Configuration of Blade Cascade in Axial Compressors;
轴流压气机叶栅新型气动布局结构的研究
2.
Aerodynamic configuration design for a parameterized lifting body common aero vehicle
通用大气飞行器的参数化气动布局研究
3.
Study of Aerodynamic Configuration Design for Buoyancy-lifting Vehicle in Near-space
临近空间浮升一体化飞行器气动布局研究
4.
Investigation of Aerodynamic Configuration Design Method for Canard Guided Projectile
鸭式制导炮弹气动布局参数设计方法研究
5.
Optimization design of aerodynamic configuration for hypersonic cruise vehicle based on ant colony algorithm
基于蚁群算法的高超声速飞行器气动布局优化设计
6.
Research on aerodynamic configuration optimization of integral performance for hypersonic cruise vehicle
高超声速飞行器气动布局总体性能优化设计研究
7.
The Derivation,Development of Weissman Chart and Applications on Configuration Design of Reentry Vehicle
Weissman图的产生、发展及其在再入航天飞行器气动布局设计中的应用
8.
Finally, an overview of aerodynamic design work on new configurations is given.
最后概述了新布局气动设计工作。
9.
The Influence of Forward-swept Agnle on the Longitudinal Characteristics of Aerodynamic Configuration with Forward-swept Wing
前掠角对前掠翼布局气动性能的影响
10.
Multidisciplinary optimization of control-aerodynamic-stealth for flying wing aircraft design
飞翼布局飞机控制/气动/隐身多学科优化设计
11.
Experimental investigation on the aerodynamic characteristics of biplane micro-air-vehicles
双翼布局微型飞行器气动特性试验研究
12.
Lateral Inject Active Vortex Control Based on Low Aspect Ratio Flying Wing
小展弦比飞翼布局飞机横向涡流控制气动机理
13.
Analyzing Lateral and Directional Static Derivatives of Flying Wing Based on Conceptual Design
飞翼布局横航向气动导数的总体估算方法研究
14.
Structural Layout Optimization of Aircraft Wing under Aeroelastic Constrains
考虑气动弹性约束的机翼结构布局优化设计
15.
Flow Mechanism of the Influence of Forward-Swept Angle on the Longitudinal Characteristics of Aerodynamic Configuration with Forward-Swept Wing
机翼掠角对前掠翼布局气动性能影响的流动机理
16.
Aerodynamics prediction and configuration optimizati on for reentry vehicle with double-ellipse cross-section
双椭圆截面再入飞行器的气动计算及布局优化设计
17.
Structure Layout and Vane Aerodynamics Analysis on Ducted Fan UAV;
涵道风扇式无人机结构布局及其叶片空气动力学分析
18.
The Influence of Different Tail Structure of Canard-missile to Missile-rolling and Other Aerodynamic Characteristics;
鸭式布局不同尾翼结构对弹箭滚转及其它气动特性的影响