Add to ORKGThe development of modern axial compressors has already reached a high level. Therefore an enlargem...
Test results are presented for 19 cascades involving five plain and two tandem blade sections. High ...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...
Performance of tandem turbine blade and its influence on flow separation and visualizatio
A jet-flap blade was designed for a velocity diagram typical of the first-stage stator of a jet engi...
Design and performance of very low-solidity turbine stator blades for first stage jet engine turbine...
The flow characteristics of several tandem bladed compressor stators were analytically evaluated ove...
With the inception of low aspect ratio blades in high pressure ratio axial compressors of modem day ...
Wind tunnel measurements, blade motions, and blade air loads for tandem-rotor helicopter
Jet engine manufacturers and designers are seeking for lighter and smaller type of axial compressors...
The purpose of NASA Research Grant NSG-3264 is to characterize the flowfield about an airfoil in a c...
Turbomachinery blade designs are becoming more aggressive in order to achieve higher loading and gre...
Surface diffusion and loading effectiveness parameters examined to increase turbine blade loadin
The results of the tandem blade configuration design study are reported. The three stage constant-in...
The problem of flow separation from a low pressure turbine blade was investigated. The operating con...
The development of modern axial compressors has already reached a high level. Therefore an enlargem...
Test results are presented for 19 cascades involving five plain and two tandem blade sections. High ...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...
Performance of tandem turbine blade and its influence on flow separation and visualizatio
A jet-flap blade was designed for a velocity diagram typical of the first-stage stator of a jet engi...
Design and performance of very low-solidity turbine stator blades for first stage jet engine turbine...
The flow characteristics of several tandem bladed compressor stators were analytically evaluated ove...
With the inception of low aspect ratio blades in high pressure ratio axial compressors of modem day ...
Wind tunnel measurements, blade motions, and blade air loads for tandem-rotor helicopter
Jet engine manufacturers and designers are seeking for lighter and smaller type of axial compressors...
The purpose of NASA Research Grant NSG-3264 is to characterize the flowfield about an airfoil in a c...
Turbomachinery blade designs are becoming more aggressive in order to achieve higher loading and gre...
Surface diffusion and loading effectiveness parameters examined to increase turbine blade loadin
The results of the tandem blade configuration design study are reported. The three stage constant-in...
The problem of flow separation from a low pressure turbine blade was investigated. The operating con...
The development of modern axial compressors has already reached a high level. Therefore an enlargem...
Test results are presented for 19 cascades involving five plain and two tandem blade sections. High ...
Present day military aero-gas turbines demand higher stage loadings for turbines so as to meet the ...