Research on the optimization design of integrated scramjet /airframe

Research on combustion efficiency of cavity-type ramjet

Secondary flow analysis for non-axisymmetric endwall on the high-load compressor cascade

Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air

Investigation of mode transition in a dual mode supersonic combustor with hydrogen fuel

School of Power and Energy,Northwestern Polytechnical University

College of Aerospace and Materials Engineering, National University of Defense Technology

Graduate University of Chinese Academy of Sciences

Institute of Engineering Thermophysics, Chinese Academy of Sciences

National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics, School of Jet Propulsion,Beijing University or Aeronautics and Astronautics