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Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A detailed two-component LDV mapping of the flow through a controlled diffusion compressor cascade at low Mach number ( ~ 0.25) and Reynolds number of about 7 × 105 , at three inlet ...
Closure to “Discussion of ‘Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence’” (1990, ASME J. Turbomach., 112, p. 266)
Publisher: The American Society of Mechanical Engineers (ASME)
Measurements of the Flow From a High-Speed Compressor Rotor Using a Dual Probe Digital Sampling (DPDS) Technique
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The flow from a high-speed rotor in a rotor-first arrangement has been measured using a “dual-probe, digital sampling (DPDS)” technique. The flow field was found to be steady in rotor coordinates ...
Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The midspan section of a previously reported controlled-diffusion compressor stator has been experimentally evaluated in cascade. Measurements were taken over a range of incidence angles for blade ...
Wake Measurements and Loss Evaluation in a Controlled Diffusion Compressor Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The results of two component laser-Doppler velocimeter (LDV) surveys made in the near wake (to one fifth chord) of a controlled diffusion (CD) compressor blade in a large-scale cascade wind ...
Stator-Averaged, Rotor Blade-to-Blade Near-Wall Flow in a Multistage Axial Compressor With Tip Clearance Variation
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper describes the effect of tip clearance changes on the pressure at the case wall of a second-stage rotor. Wall shear distributions under the rotor tip are also presented. The results ...
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