Dissertation > Excellent graduate degree dissertation topics show

Aeroengine full state modeling technology

Author: ZhangJian
Tutor: HuangJinQuan
School: Nanjing University of Aeronautics and Astronautics
Course: Aeronautical and Astronautical Science and Technology
Keywords: Turbofan engine Component -level model Start Modeling Vectoring nozzle Adjustable guide vane angle
CLC: V231
Type: Master's thesis
Year: 2009
Downloads: 295
Quote: 1
Read: Download Dissertation

Abstract


Related Dissertations

  1. The turbofan engine pneumatic runner Optimization Approach,V235.13
  2. Vectoring nozzle axis of symmetry of DSP - based digital control system design techniques,TK403
  3. Numerical Study of the High Speed Main Flow and Thrust Vectoring Interaction,V211.4
  4. Design Rules of Dual-throat Fluidic Thrust-vectoring Nozzle and Its Integration with the Afterbody of Aircraft,V228.73
  5. Modeling and Simulation of Aeroengines Based on MATLAB,V231
  6. X turbofan engine transition state optimizing control,V233.7
  7. Standoff Airborne Dispenser overall design of key technologies,E926.4
  8. Vectoring nozzle control kinematics modeling and integrated engine control study,V233.7
  9. The turbofan engine Variable Geometry and Stable and optimization analysis,V235.13
  10. The Research on Turbo-fan Aeroengine Adaptive Modeling,V235
  11. Performance Calculation of Uniaxial Turbofan Engine,TK402
  12. Study on the Design of Turbofan Engine Control System,V235.1
  13. Optimization of Turbofan Engine Acceleration Control Law,V235.13
  14. Numerical simulation of the turbofan engine start,V235.13
  15. Turbine based combined cycle engine integration performance numerical simulation,V235
  16. Research on Aerodynamic Characteristics of Counterflow Thrust Vectoring Nozzle,V231.3
  17. Design and Performance Simulation of an Experimental Rig for Infrared Stealth Research of Exhaust System of a Turbofan Engine,V231.1
  18. Development on Six-component Balance System for Measuring Plane Engine Vector Nozzle,V263.3
  19. Aerodynamic Design and Analysis for Low Pressure Turbine of a Large Scale Turbofan Engine,V235.13
  20. Component-based modeling and fault simulation of aircraft auxiliary air conditioning system troubleshooting troubleshooting simulation training and research,V245.34

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