A methodology was proposed to develop generic aero-engine simulation platform by using software componentization.From the point of view of the engine construction engine model was broken down into several components
from the point of view of software functions the supplementary part of the simulation software was also broken down into multiple components.And a simulation platform of turbofan engines was established
which had achieved good effect.The simulation system based on this method had achieved to be modular
hierarchical
and easy to be maintained and improved.It has strong expandability
and has increased code reuse rate
which reflects the flexibility of the framework of the simulation platform.
Research of object-oriented general aero-engine modeling techniques
Whole flight envelop corrected equilibrium manifold modeling for a turbofan engine
Aero-Engine State Variable Modeling Based on the Genetic Algorithm
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Related Author
HU Wei-bo
CHENG Bang-qin
CHEN Zhi-min
ZHAO Hang
LI Shu-qing
ZHANG Sheng-xiu
HU Wei-hong
LI Qiu-hong
Related Institution
Aeronautics and Astronautics Engineering College, Air Force Engineering University
Staff Room 303,The Second Artillery Engineering College
The Second Artillery Military Delegation in the 31st Research Institute, The Chinese People's Liberation Army
College of Energy &amp Power EngineeringNanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics