V22,Aircraft Construction and Design

About 668 item dissertation in line with V22,Aircraft Construction and Design query results,the following is 1 to 50(Search took 0.021 seconds)

Design and Control Research of Ducted Fan Micro Air Vehicle,CaiHongMing/Nanjing University of Aeronautics and Astronautics,0/29
Tailless Morphing Wing Aircraft Mechanism Design and Aerodynamic Analysis,DuXia/Nanjing University of Aeronautics and Astronautics,0/45
Numerical Simulation of Oxygen Distribution in Aircraft Fuel Tank Ullage and Theoretical and Experimental Study of Airflow Optimization,LuShiHua/Nanjing University of Aeronautics and Astronautics,0/10
Optimaldesignand Mechanical Analysis of the Variable Sweep Wings Structure,ZhangJian/Harbin Institute of Technology,0/125
Design of Lightweight Landing Gear Based on Magnetorheological Damper and Damping Performance Research,JiangZheZhu/Harbin Institute of Technology,0/106
Research on the Knowledge Acquisition and Reuse Method Oriented to Aircraft Structure Design,YangXuGuang/Harbin Institute of Technology,0/69
Research on the Actuation Technology of Variable Height and Cant Winglet,LiWei/Nanjing University of Aeronautics and Astronautics,0/10
Research of Stochastic Stability and Reliability on the Casing Pipe of Flying Boom,YaoShiLei/Tianjin University,0/7
Numerical Simulation of Reasonable Row Number for an Aircraft Cabin and the Contaminant Transportation,LiuSuMei/Tianjin University,0/3
Research on Assessment Method of Min Crew Workload Application to Civil Aircraft Cockpit,LiuShuQiang/Nanjing University of Aeronautics and Astronautics,0/6
Research on Optimization Design Method of Aircraft Overall Parameters and Trajectory,ChenYangYang/Harbin Engineering University,0/73
Numerical Simulation of Mixing Ventilation in a Commercial Airliner Cabin,WuChen/Tianjin University,0/8
Waverider Aerodynamic Configuration Design and Numerical Simulation Validation,ZhaoBo/Harbin Engineering University,0/55
Theoretical and Experimental Study on the Leading-edge Tubercle of Three-dimensional Airfoil,ChengXiangRu/Harbin Engineering University,0/31
The Layout Optimization Study for Civil Aircraft Cockpit Ergonomics Design,NiuSong/Nanjing University of Aeronautics and Astronautics,0/38
Research on Evaluation Method of the Cockpit Ergonomics for Civil Aircraft,LiuQiYue/Nanjing University of Aeronautics and Astronautics,0/53
Research on the Integration for Aircraft Stable Equipment,YuanZuo/Nanjing University of Aeronautics and Astronautics,0/3
Study on Airfoil Design and Influence of Tip Clearance of High Subsonic Micro Axial Turbine,DengYang/Nanjing University of Aeronautics and Astronautics,0/7
Highly Accurate Aerodynamic Shape Opitmization with a Large Number of Design Parameters Based on a New and Efficient Global Opitmization Algorithm,WuWenHua/China Aerodynamics Research and Development Center,0/114
Studyon Design Method and Performance Simulationof Lubrication Systemfor Helicopter Transmission,YangHuiDong/Central South University,0/33
A Fuzzy Controller Design for Aircraft Anti-Skid Braking System Based on Particle Swarm-Optimization Algorithm,DengZuoXi/Central South University,0/12
Design of Hardware-In-The-Loop Simulation Platform for Aircraft Braking System Based on LabVIEW,BianJing/Central South University,0/26
Research and Design of Integrated Controller of Main Wheel Braking System and Nose Wheel Steering System in Aircraft,LiuZhengHui/Central South University,0/14
Research on Mechanism Motion Reliability and Parameter Sensitivity on a Type of Landing Gear,YinZuo/Central South University,0/30
Structural Research of the Segmented Morphing Wing Based on the SMA Modular Actuator,ChenZhongYuan/Central South University,0/24
FEM Analysis of Telescoped Morphing Wingand Hydraulic System Design,JiaPeng/Beijing University of Technology,0/47
The Design of Aircraft Fuel Accessory Testing System and the Research of Its Decoupling Algorithm,WangXiangPeng/Qingdao University of Science and Technology,0/3
Human-Centered Design Analysis and Research on the Design of Aircraft Seat for Children,WangKun/Qingdao Technological University,0/37
Numerical Simulation of Pollutants Transport in An Aircraft Cabin,MuXiaoHong/Nanjing University of Technology and Engineering,0/9
Development and Simulation of the Dynamic Seals Test System for Aircraft Cylinders,LiuBen/Zhejiang University,0/29
Hypersonic Flight Vehicle Aerodynamic Parameters Identification and Input Design Technology Research,LiChao/Xiamen University,0/4
The Research of Numerical Simulation of Grid Fins with Different Forward-swept and Back-swept Angles and Airfoil Profile,XiYuan/University of North,0/3
The Key Strength of Aircraft Landing Gear Components Analysis and Structural Optimization,YaoGuangSheng/University of North,0/10
Thermo-structural Analysis and Design of Hypersonic Vehicle Leading Edge,ZhangYu/Harbin Institute of Technology,0/54
Performance Study of Composite Mechanically Fastened Joints and Joint Design,XieYongGang/Harbin Engineering University,0/107
Aerodynamic Design of Bleed Flow Turbine Integrated on Hypersonic Near Spacecraft,LvShouQing/Harbin Institute of Technology,0/4
Design for Thermal Structure of Flight Vehicle and Thermal-stress Analysis,CaiZhen/Harbin Institute of Technology,0/7
Digital Cockpit Fault Tolerant Control Panel System Based on ARINC825,ZhangPengYu/Harbin Institute of Technology,0/6
Study on Numerical Simulation of Air-flow Based on Aircraft Cabin,HuangYanZuo/Chongqing University,0/0
Design and Study on3-bearing Swivel Duct Nozzle,ZhangYiJun/Lanzhou Jiaotong University,0/2
Numerical Calculation and Research of Temperature Field of Brake for Aircraft during Braking,JianZhengZhu/Central South University,0/36
Study of non electric vacuum liquid circulation system,LeiChunNiu/University of North,0/12
The Time Characteristics and Optimization Method in Aircraft Design Process,XuLiNa/Shenyang Aerospace University,0/35
The Simulation and Experiment Study on Aircraft Hydraulic Tubes’ Quick Maintenance,LiChangQing/Shenyang Aerospace University,0/35
Safety Evaluation of the Wing by Finite Element Method,ZhangJing/Shenyang Aerospace University,0/37
Research on Static and Dynamic Characteristics of the Variable Wing Based on the Optical Fiber Sensing System,WangXiaoGang/Nanjing University of Aeronautics and Astronautics,0/47
Research of Rotary Bending Fatigue Test for No Flaring Connection of Aviation Conduit,ShuSong/Shenyang Aerospace University,0/49
Study on Separation Performance of Onboard Hollow Fiber Membrane and Flush Inerting for Fuel Tank of Civil Aircraft,XueYong/Nanjing University of Aeronautics and Astronautics,1/39
Research on the Calculation of Transient Heat Load of Aircraft Cabins,XiaZuoZuo/Nanjing University of Aeronautics and Astronautics,0/64
Research on Trailing with Compliant Mechanism and Topological Optimization Based on the Load Path,WangZuo/Nanjing University of Aeronautics and Astronautics,1/46