Single stage experimental evaluation of slotted rotor and stator blading. Part III - Data and performance for slotted rotor 1
Effect of slots on performance of highly loaded compressor rotor blades
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Experimental evaluation of transonic stators, data and performance report, multiple- circular-arc stator A
Transonic stator with multiple circular arc airfoils and minimum curvature tested over range of flow angles and velocities - stator A
Bogardus, G. A.↗
Experimental evaluation of transonic stators, data and performance report, multiple circular arc stator B
Transonic stator with multiple circular arc airfoils and minimum curvature tested over range of flow angles and velocities - stator B
Bartok, J. A.↗
Experimental Evaluation of Transonic Stators, Data and Performance Report, Double Circular Arc Stator
Transonic stator with double circular arc airfoils tested over range of flow angles and velocities
Bartok, J. A.↗
Experimental evaluation of transonic stators. Data and performance report multiple- circular-arc stator A /slotted/
Multiple circular-arc slotted stator for transonic speed operation
Bartok, J. A.↗
Single-Stage Experimental Evaluation of Boundary Layer Blowing Techniques for High Lift Stator Blades. III - Data and Performance of Single-Slotted 0.65 Hub Diffusion Factor Stator
Test on overall and blade element performance of single slotted 0.65 hub diffusion factor stator with self energized blowing boundary layer control
Miller, M. L.↗
Single stage experimental evaluation of variable geometry guide vanes and stator blading. Part 3 - Data and performance for variable camber guide vane and stator A
Performance tests of variable camber guide vane and stator to extend range of axial flow compressors
Jones, B. A.↗
Single-stage experimental evaluation of boundary layer blowing techniques for high lift stator blades. 4 - Data and performance of double-slotted 0.75 hub diffusion factor stator
Boundary layer hub diffusion-factor stator blowing technique
Carmody, R. H.↗
Single-stage experimental evaluation of boundary layer bleed techniques for high lift stator blades. Part 3 - Data and performance of unslotted 0.75 hub diffusion factor stator
Boundary layer bleed techniques for high lift compressor stator blades
Carmody, R. H.↗
Single-stage experimental evaluation of boundary layer bleed techniques for high lift stator blades. Part 4 - Data and performance of triple-slotted 0.75 hub diffusion factor stator
Performance tests on slotted hub diffusion factor stator with boundary layer bleed
Carmody, R. H.↗
High-loading low-speed fan study. Part 2 - data and performance unslotted blades and vanes
Aerodynamic performance, and noise measurements of highly loaded low speed fan
Burdsall, E. A.↗
Single-stage evaluation of highly-loaded high- Mach-number compressor stages. 3 - Data and performance tandem rotor
Characteristics of highly-loaded, high Mach number, single stage compressor
Burger, G. D.↗
Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Task 2 stage data and performance report
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 1
Bilwakesh, K. R.↗
Undistorted inlet flow testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Task 2 stage data and performance report
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 2
Bilwakesh, K. R.↗
Inlet flow distortion testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Task 2 stage data and performance report
Inlet flow distortion testing of high Mach number transonic fan stages - Vol. 1
Doyle, V. L.↗
Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1
Test description and results for high Mach number transonic fan stages to determine range and distortion tolerance for various rotor tip casing treatment configurations
Tesch, W. A.↗
High-loading low-speed fan study. 3 - Data and performance slotted blades and vanes and rotor tip treatment
Slotted blades and vanes and rotor tip design for highly loaded, low speed fan stage applicable to low noise aircraft engines
Burdsall, E. A.↗
Single stage evaluation of highly loaded high Mach number compressor stages. 4: Data and performance of hub slit suction stator
Performance tests and efficiency measurement of hub-slit-suction stator in single stage compressor
Burger, G. D.↗