Dissertation 

About 77 item dissertation in line with China Aerodynamics Research and Development Center query results,the following is 1 to 50(Search took 0.046 seconds)

  1. Numerical Study on Air Throttling Influence on the Performance of Combustion in the Scramjet Combustor,TianYe/China Aerodynamics Research and Development Center,0/9
  2. Aerodynamics, Aerothermodynamics and Heat-Transfer Investigation for Mars Entry Vehicles,YangXiaoFeng/China Aerodynamics Research and Development Center,0/24
  3. Study on Reentry Trajectory Design and Guidance Approach for Lifting Spacecraft,ZhengFengZuo/China Aerodynamics Research and Development Center,0/63
  4. 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
  5. Study on the Similarity Criteria and Simulation Method of the Wind Tunnel Based Virtual Flight Testing,LiHao/China Aerodynamics Research and Development Center,0/140
  6. Investigation on Dynamic Derivative Test Technique in Φ1m Hypersonic Wind Tunnel,GuoLeiTao/China Aerodynamics Research and Development Center,0/46
  7. Investigation on Aerodynamic Characteristics of Internal Weapons Bay System,WuJiFei/China Aerodynamics Research and Development Center,0/74
  8. Investigation of the Numerical Simulation on Porpeller/Wind Turbine Using Steady and Unsteady Methods,YangXiaoChuan/China Aerodynamics Research and Development Center,0/84
  9. Research on High Speed Static Aeroelastic Model Design of High-Aspect-Ratio Wing,KouXiPing/China Aerodynamics Research and Development Center,0/80
  10. Research of Reynolds Number Effects for Shock-Induced Separations on Supercritical Airfoils,XuXin/China Aerodynamics Research and Development Center,0/42
  11. High Order DG/FV Hybrid Method on Hybrid Grid,LiMing/China Aerodynamics Research and Development Center,0/78
  12. Investigation of Implicit Time Integration Methods with HDCS Schemes,YanZhenGuo/China Aerodynamics Research and Development Center,0/57
  13. Investigations on the High-order Finite Difference Schemes and Numerical Simulations on the Aeroacoustic Characteristics of Mixing Layers,GuoQiLong/China Aerodynamics Research and Development Center,0/54
  14. The Investigation of the Massively Separated Flow and Vortical Flow on the Leeward Side of Double-Delta Wing by Using Detached-Eddy Simulation,SunDong/China Aerodynamics Research and Development Center,0/72
  15. Numerical Computation of Aircraft Icing and Study on Icing Test Scaling Law,YiXian/China Aerodynamics Research and Development Center,21/684
  16. Numerically Simulate Aero-Force&Heat of Hypersonic Vehicles and Region Marching Method for Supersonic Flow Simulation,HeXuZhao/China Aerodynamics Research and Development Center,8/1945
  17. Applications of Chemical Equilibrium and Flamelet Model for the Numerical Simulation of Scramjet,XingJianWen/China Aerodynamics Research and Development Center,9/570
  18. Investigation of Computational Modeling Techniques for Rotor Flowfields,XiaoZhongYun/China Aerodynamics Research and Development Center,7/1003
  19. Parallel Numerical Simulations of the Whole Scramjet Engine Flowfields on Unstructured Grids,WangLan/China Aerodynamics Research and Development Center,12/835
  20. Numerical Simulation of Hypersonic and High Temperature Gas Flowfields,LiHaiYan/China Aerodynamics Research and Development Center,8/1470
  21. Numerical Investigation on the Unsteady Separation Flows Around Double-Delta Wings,ChenLiangZhong/China Aerodynamics Research and Development Center,1/397
  22. Development of Numerical Method and Investigation on Performances of Supersonic Ejectors,LiuHuaYong/China Aerodynamics Research and Development Center,3/481
  23. Investigations of Convergence Acceleration and Complex Flow Numerical Simulation for High-Order Accurate Scheme (WCNS),ZhangYiFeng/China Aerodynamics Research and Development Center,4/313
  24. Stability Analysis of Supersonic Boundary Layers and High Order Shock-Capturing Schemes,TuGuoHua/China Aerodynamics Research and Development Center,1/498
  25. Numerical Simulation of Aerodynamic Characteristics for Micro Air Vehicles,SongShuHeng/China Aerodynamics Research and Development Center,0/399
  26. Large Eddy Simulation of Incompressible Turbulent Flow,DengXiaoBing/China Aerodynamics Research and Development Center,2/1311
  27. Investigation on the Mechanism and Reynolds Number Effect on Flow Asymmetry at High Incidence,WangYuanJing/China Aerodynamics Research and Development Center,0/259
  28. Discontinuous Galerkin Finite Element Method on Hybrid Grids and Finite Element/Finite Volume Mixed Method,HeLiXin/China Aerodynamics Research and Development Center,1/428
  29. Study on Heat Transfer Characteristics and Effects of Electrothermal Aircraft Deicing,XiaoChunHua/China Aerodynamics Research and Development Center,0/107
  30. Studies on Aeroacoustic Characteristics and Noise Suppressions for Internal Weapon Bays,YangDangGuo/China Aerodynamics Research and Development Center,0/157
  31. Implementation of Reduced Chemical Kinetics of Hydrocarbon Fuels and in Situ Adaptive Tabulation in Parallel Computations of Supersonic Combustion,XiaoBaoGuo/China Aerodynamics Research and Development Center,0/140
  32. Investigation of Control Surface Hinge Moment Characteristic at Low Speed,HuangZongBo/China Aerodynamics Research and Development Center,2/134
  33. Numerical and Experimental Research for the Ignition Delay Time of the Ethylene in the Scramjet,WangXiYao/China Aerodynamics Research and Development Center,1/133
  34. A Study on One-Dimensional Method for Combustion Efficiency Evaluation and Influence Factors Effect Analysis,WangZhenFeng/China Aerodynamics Research and Development Center,2/149
  35. Design of Configuration and Research of Aerodynamic Performance for Waverider Vehicles,DangLeiNing/China Aerodynamics Research and Development Center,5/318
  36. Application and Study on Numerical Algorithm of the Boltzmann Model Equation in Channel Flow,BiLin/China Aerodynamics Research and Development Center,0/225
  37. Unsteady Numerical Method Based on Dynamic Hybrid Mesh and Simulation of Bio-fluid Flows,ChangXingHua/China Aerodynamics Research and Development Center,1/150
  38. Study and Applications of High-order Accurate Dissipative Compact Schemes,LiSong/China Aerodynamics Research and Development Center,1/203
  39. Study of Turbulence-degraded Image Restoration Technology Based on Fractional Fourier Transform,CaoDong/China Aerodynamics Research and Development Center,1/98
  40. Primary Discuss of Icing Wind Tunnel Cloud Parameters Variation Law,HuZhanWei/China Aerodynamics Research and Development Center,0/198
  41. Comparative Evaluation of Unsteady Aerodynamic Mathematic Models of Aircraft,ZhangHaiYou/China Aerodynamics Research and Development Center,0/169
  42. The Study of Parameter Estimation for Turbulence Model,ZhouYu/China Aerodynamics Research and Development Center,1/242
  43. Research of Second Throat Design of Continuous Transonic/Supersonic Wind Tunnel,QinHongGang/China Aerodynamics Research and Development Center,1/69
  44. Research of Corner Vanes Technique on Low Pressure Loss,YiXingYou/China Aerodynamics Research and Development Center,0/111
  45. Numerical Simulation of the Dynamic Aerodynamic Characteristics about Partial Flexible Airfoils and Folding Wing Aircraft,GuoQiuTing/China Aerodynamics Research and Development Center,3/487
  46. Numerical Study of the Pitching Motion of Vehicles and the Rudder Control,ChenZuo/China Aerodynamics Research and Development Center,0/160
  47. Application and Study on High Order Scheme of Gas Kinetic for Solving the Boltzmann Model Equation,PengAoPing/China Aerodynamics Research and Development Center,0/97
  48. Quasi-One-Dimensional Theoretical Analysis of Ejector Mode of Rocket-Based Combined Cycle Engine,LinQi/China Aerodynamics Research and Development Center,1/116
  49. Pilot Study of Discontinuous Galerkin Methods for Euler Equations,GongXiaoQuan/China Aerodynamics Research and Development Center,0/183
  50. The Researching of Numerical Simulation Method of Aeroacoustics for Hovering Rotors of Helicopter,ChenZhengWu/China Aerodynamics Research and Development Center,0/166

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