To investigate lean-blow-out (LBO) performance of trapped vortex combustor (TVC) in high inlet flow
experiments were employed by changing Ma and temperature of main air and height to length (H/L) of the cavity.The results of experiments show that:(1) Mach number of main air has great effect on LBO.When Mach number of inlet main air becomes bigger
LBO decreases.As Mach number of inlet conditions varies
the change of LBO is great.(2) Temperature rise of main air is conducive to LBO
but after 600K
the effect is less.(3) LBO decreases when after body of cavity gas amount becomes bigger.(4) When the H/L is 0.88
Research on combustion efficiency of cavity-type ramjet
Characteristics of lean blowout limit for backward step-stabilized flame with centrifugal force effect
Atomization and evaporation performance experiment of evaporating tube for trapped vortex combustor
底部凹腔加侧开孔减阻研究
某型燃烧室提高总压恢复系数改进方案设计及试验验证
Related Author
WANG Zhen-guo
PAN Yu
HUANG Guo-qing
TAN Jian-guo
SUN Qiang
GUO Xin-hua
LIN Yu-zhen
LI Lin
Related Institution
College of Aerospace and Materials Engineering, National University of Defense Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-therodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics