Dissertation > Excellent graduate degree dissertation topics show

Tapered flow characteristics of isolation

Author: TianXuAng
Tutor: ChengKeMing
School: Nanjing University of Aeronautics and Astronautics
Course: Fluid Mechanics
Keywords: Aerodynamic flow Variable cross-section isolator Pseudo- shock train Shock train Ramjet
CLC: V231.3
Type: Master's thesis
Year: 2008
Downloads: 121
Quote: 3
Read: Download Dissertation

Abstract


Related Dissertations

  1. The turbofan engine pneumatic runner Optimization Approach,V235.13
  2. Numerical Simulation of Flow Fields in a Ramjet Isolator with a Divergent Angle,V235.21
  3. Stamping extended-range rockets integration of internal and external ballistics calculation,TJ415
  4. The solid fuel stamping extended-range missile integration of internal and external ballistic computing research,TJ413
  5. Design of Key Components and Performance Assessment Test for Ramjet Combustor,V235.21
  6. Experiment and Numerical Simulation on the Inlet’s Flow Field of Ramjet Pill Assisted Range Projectiles,TJ413
  7. Working Process Simulation and Performance Analysis for Solid Fuel Ramjet Projectile,TJ413
  8. Structural integrity analysis of solid fuel stamping extended-range missile,TJ413
  9. Research on Form Surface Aerodynamic Optimization Method of Ramjet Assisted Range Projectile Inlet,TJ413
  10. Numerical Simulation and Experimentation Research on Vortex Enhancing Combustion of Solid Fuel Ramjet,V435
  11. Experimental Technology Study of the Inlet in Hypersonic Pulse Wind Tunnel,V211.74
  12. Gas flow adjustable dynamic response of solid rocket ramjet Process,V435
  13. Study on Virbartion Characteristic of Panel Structures of Ramjet Inlet Affected by High Speed Fluid Flows,V215.34
  14. Investigation of Streamwise Vortex Enhanced H2/Air Mixing in a Gaseous Hydrogen Fueled Ramjet,V438
  15. Primary Research of New Conceptive Internal-Rotor Burnt Rotating Ramjet,V235
  16. Aerodynamic Performance Analysis of Scramjet Isolator under Asymmetric Supersonic Flow,V237
  17. Integrated Design of Integral Rocket-Ramjet Missile,TJ760
  18. Vehicle overall optimal design theory and application,V221
  19. Theoretical and Experimental Research on the Operation Process of the Solid Fuel Ramjet,V435
  20. Investigation on the Working Process of Solid Fuel Ramjet,V435

CLC: > Aviation, aerospace > Aviation > Aero-engine ( propulsion system ) > Engine theory > Aero-engine gas mechanics
© 2012 www.DissertationTopic.Net  Mobile