Numerical Simulation of Steady and Transient Working Progress in Aviation Gas Turbine Engine-Reference-Cited by-同舟云学术

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Numerical Simulation of Steady and Transient Working Progress in Aviation Gas Turbine Engine

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2009 Conference & Exposition
language:
Short-container-title:

Author:

Chang Zhong-hong¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6657

Reference5 articles.

1. 1Nigmatullin M. Ja. Ivanov and R.Z. Interconnected Multi-Level Design of Gas Turbine Elements [R].AIAA2003-12152003.

2. 21D unsteady code for gas flow calculation through gas turbine engine flow passage User's guide [Z],CIAM(CentralInstituteofAviationMotors),2005.

3. 3MauriceHolt,ReviewofGodunovMethods,NASACR-198322.

4. 4HirschCharles:NumericalComputationofInternalandExternalFlows,vol.I:Fundamentalsof Numerical Discretization,Wiley, NewYork,1988.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Wireless Technologies Modular Construction of Aviation Gas Turbine Engines;2023 IEEE 7th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC);2023-10-24

2. Power Balance Strategies in Steady-State Simulation of the Micro Gas Turbine Engine by Component-Coupled 3D CFD Method;Aerospace;2023-09-04

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