机译:在风冷燃气轮机叶片设计中最小化局部熵产生率
机译:Effect of local mistuning of blade vibration frequencies on the vibration stress of compressor and turbine disks of aircraft gas turbine engines
机译:An analytical method of fatigue damage estimation for compressor stator blades of gas turbines under rotating stall (1st report, residual life assessment of gas turbine compressor blades)
机译:A Methodology to Synthesize Gearbox and Control Design for Increased Power Production and Blade Root Stress Mitigation in a Small Wind Turbine
机译:Degradation and recovery of material properties on gas turbine blades
机译:ssmE alternate Turbopump Development program (HpFTp): Verification complete report second turbine blade aerodynamic design DVs DR No. 3.1.2.2.4.1, Vm No. 4.1.2.4 a