Results 11 to 20 of about 302,000 (307)
Xibei Gongye Daxue Xuebao, 2021 By experiment at a low-speed large-scale axial contra-rotating compressor, the near stall points of 19 speed configurations were captured and the stall characteristics under different speed ratios were obtained successfully.
Wang Hao +3 more
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Method of Improving Stability of a Highly-Loaded Axial Compressor Stage by Coupling Different Casing Treatments [PDF]
Journal of Applied Fluid Mechanics, 2022 Casing treatment is a powerful method for improving the stability of aircraft compressors. An optimized slot-type casing treatment was tested on the first rotor of a highly-loaded two-stage compressor, and the results showed that the casing treatment ...
Y. Chen, A. Lin, H. Zhang, W. Chu
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Energies, 2021 The RANS (Reynolds-averaged Navier–Stokes equations) with CFD (Computational Fluid Dynamics) simulation method is used to analyze the head hump formation mechanism in the double-suction centrifugal pump under a part load condition.
Yong Liu +5 more
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Propagation of stall in a compressor blade row [PDF]
, 1955 Recent experimental observations on compressors, in particular those of Rannie and Iura, have clarified some features of the phenomenon of stall propagation.
Marble, Frank E.
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Delaying the Stall of A Low-Wing Aircraft Using A Novel Powerful Vortex Generator
Inventions, 2022 In this study, a new aerodynamic surface concept is introduced, which is a powerful vortex generator (PVG). It can delay the stall point in a low-wing aircraft. This delay leads to a significant increase in the CLmax of an aircraft.
Mostafa Goharshadi, Masoud Mirzaei
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Boundary Layer Separation and Reattachment Detection on Airfoils by Thermal Flow Sensors
Sensors, 2012 A sensor concept for detection of boundary layer separation (flow separation, stall) and reattachment on airfoils is introduced in this paper. Boundary layer separation and reattachment are phenomena of fluid mechanics showing characteristics of ...
Peter Busche +4 more
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Detection and Analysis of an Alternate Flow Pattern in a Radial Vaned Diffuser
International Journal of Turbomachinery, Propulsion and Power, 2020 The flow in the vaned diffuser of an aeronautical centrifugal compressor designed by Safran Helicopter Engines is analyzed through steady and unsteady pressure measurements at different rotation speeds.
Victor Moënne-Loccoz +3 more
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Determination of Ranges of Unstable Operation of Axial Compressor for Aircraft Turbine Engines [PDF]
Problemy Mechatroniki, 2022 Currently, strict requirements are set for aircraft turbine engine performance, which requires introducing larger, more complex, and more loaded compressors.
Adam KOZAKIEWICZ +2 more
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Journal of Parallel and Distributed Computing, 2005 zbMATH Open Web Interface contents unavailable due to conflicting licenses.
BILARDI, GIANFRANCO +3 more
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Applied Sciences, 2020 A numerical study was conducted on the influence of turbulence intensity and Reynolds number on the mean topology and transition characteristics of flow separation to provide better understanding of the unsteady jet flow of turboelectric distributed ...
Yang Zhang, Zhou Zhou, Kelei Wang, Xu Li
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