Effect of steady-state pressure distortion on flow characteristics entering a turbofan engine [PDF]
Flow angle, static-pressure, and total-pressure distributions were measured in the passage ahead of a turbofan engine operating with inlet pressure distortion.
Bobula, G. A., Soeder, R. H.
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Application of Digital Twins and Metaverse in the Field of Fluid Machinery Pumps and Fans: A Review. [PDF]
Yang B+4 more
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Effect of casing treatment of overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5 [PDF]
The effect of a number of casing treatments on the overall performance of a 1.75-pressure-ratio, 423-m/sec-tip-speed fan stage was evaluated. The skewed slot configuration with short-open slots over the midportion of the rotor had a stall margin of 23.5 ...
Moore, R. D., Osborn, W. M.
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The internal losses in the tip clearance region strongly influence the compressor performance and its operational range. Previous research proved that passive wall treatments with circumferential grooves in axial compressors effectively increase the ...
Ruben Bruno Diaz+4 more
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Investigation on the Flow Field Entropy Structure of Non-Synchronous Blade Vibration in an Axial Turbocompressor. [PDF]
Zhang M, Hou A.
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Rotating Stall in Multistage Axial Compressors : 1st Report, Small Disturbance Theory 1
Hiroyuki TAKATA, Takuro OKAZAKI
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Rotating Stall in Multistage Axial Compressors : 2nd Report, Small Disturbance Theory 2
Hiroyuki TAKATA, Takuro OKAZAKI
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Frequency response of an axial-flow compressor exposed to inlet pressure perturbations [PDF]
Experimental results of a series of engine tests designed to obtain the stage dynamics of an eight-stage axial-flow compressor over the frequency range of 0.5 to 200 hertz are presented.
Milner, E. J.+2 more
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A critical review on renewable battery thermal management system using heat pipes. [PDF]
Afzal A+5 more
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Discussion: “Experimental and Analytical Investigation of the Effects of Reynolds Number and Blade Surface Roughness on Multistage Axial Flow Compressors” (Scha¨ffler, A., 1980, ASME J. Eng. Power, 102, pp. 5–12) [PDF]
C. C. Koch, L. H. Smith
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