Add to ORKGOutlet annulus area blockage configuration effects on performance of axial flow compressor roto
Aerodynamic design parameters are presented along the overall and blade element performance, of an a...
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compresso
July 1981Includes bibliographical references (page 29)An experiment was carried out to examine the e...
Simulating downstream flow blockage doors in bypass air duct of turbofan engine with axial flow fan ...
Total-pressure deficiency for an annular cascade of 65-(12)10 blades was measured at three radial st...
The performance of the first stage of a transonic, multistage compressor was mapped over a range of ...
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The experimental performance of a 20-inch-diameter axial-flow transonic compressor rotor with small ...
A collection of noncavitating blade-element performance data for 12 axial-flow pump rotor configurat...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
Performance of vortex generators installed aft of inlet throat on centerbody evaluated at Mach numbe...
Previous performance data of the 19XB axial-flow compressor indicated that the outlet guide vanes an...
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this ...
Partial admission operation effects on performance of single stage axial flow turbin
Aerodynamic design parameters are presented along the overall and blade element performance, of an a...
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compresso
July 1981Includes bibliographical references (page 29)An experiment was carried out to examine the e...
Simulating downstream flow blockage doors in bypass air duct of turbofan engine with axial flow fan ...
Total-pressure deficiency for an annular cascade of 65-(12)10 blades was measured at three radial st...
The performance of the first stage of a transonic, multistage compressor was mapped over a range of ...
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The experimental performance of a 20-inch-diameter axial-flow transonic compressor rotor with small ...
A collection of noncavitating blade-element performance data for 12 axial-flow pump rotor configurat...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
Performance of vortex generators installed aft of inlet throat on centerbody evaluated at Mach numbe...
Previous performance data of the 19XB axial-flow compressor indicated that the outlet guide vanes an...
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this ...
Partial admission operation effects on performance of single stage axial flow turbin
Aerodynamic design parameters are presented along the overall and blade element performance, of an a...
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compresso
July 1981Includes bibliographical references (page 29)An experiment was carried out to examine the e...