Prediction of civil aircraft emission in complete flight route
Experimental study on lean-blow-out of double/fuel-lean trapped vortex combustor
Characteristics of lean blowout limit for backward step-stabilized flame with centrifugal force effect
AN OPTIMIZATION METHOD FOR STATISTICAL ASCERTAINMENT OF THE MOST PROBABLE PEAK TEMPERATURE AT COMBUSTOR EXIT
Related Author
曾文
曹隽华
许如意
刘凯
ZHANG Xiao-bo
LIU Zeng-wen
WANG Zhan-xue
CAO Ming-dong
Related Institution
School of Power and Energy,Northwestern Polytechnical University
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institue, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-therodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics