Over/under type inlet scheme for turbine-based combined cycle engine
Research on variable geometry technology of 2-D hypersonic inlet with contract ratio under controlling
Numerical simulation on performance of variable cycle engines
Dynamic investigation on hypersonic sidewall compression inlets with cowl valve during the process of transition
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Related Author
WANG Ya-gang
YUAN Hua-cheng
GUO Rong-wei
TENG Jian
LIU Zeng-wen
WANG Zhan-xue
HUANG Hong-chao
CAI Yuan-hu
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,ChinaChina Gas Turbine Establishment,Aviation Industry Corporation of China
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology