Mr Zhe Liu

All Stories

1. 
   Numerical analysis on the effect of CTAP measurements in pulse and rotating detonation combustors

   Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

   Mr Zhe Liu, Mr Jorge Saavedra, James Braun

2. 
   Characterization of an integrated nozzle and supersonic axial turbine with a rotating detonation combustor

   Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

   James Braun, Mr Zhe Liu, Mr Jorge Saavedra

3. 
   Three Dimensional Optimization for Subsonic Axial Turbines Operating at High Unsteady Inlet Mach Number

   Article • July 2018, American Institute of Aeronautics and Astronautics (AIAA)

   Mr Zhe Liu

4. 
   Performance of axial turbines exposed to large fluctuations

   Article • July 2017, American Institute of Aeronautics and Astronautics (AIAA)

   Mr Zhe Liu