Combustion instabilities were studied experimentally by coupling unsteady heat release and pressure perturbations.In this paper
the experimental studies were conducted to analyze the dynamic processes of self-excited combustion oscillations through dynamic pressure and phase-locked chemiluminescence measurements.The effects of air mass flow
equivalence ratio and boundary conditions on combustion system were examined.This shows that the amplitudes of oscillation will enlarge with the increasing system load
leading to more unstable combustion.Moreover
the higher modes of oscillation frequency may occur when the combustion operation is closer to lean limits.
Effects of liner pressure loss on combustor ignition performances
Effects of liner pressure loss on combustor lean blow-out and combustion efficienly performances
Numerical Simulation Studies on the Discharge Coefficient of Gas Turbine Combustor Liner Air Holes
基于三维接触摩擦单元的套齿连接解析建模研究
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
Related Author
Lei JIANG
Tong WANG
Hongbin HU
Bohan WANG
Xiangyu JIANG
Sumin CHEN
DU Jiang-yi
XU Quan-hong
Related Institution
Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences
Key Laboratory of Advanced Energy and Power,Institute of Engineering Thermophysics,Chinese Academy of Sciences
Innovation Academy for Light⁃duty Gas Turbine,Chinese Academy of Sciences
School of Engineering Science,University of Chinese Academy of Sciences
National Key Laboratory of Science and Technology on Aero-Engine Aerothermodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics