Results 11 to 20 of about 299,991 (289)

RANS CFD Analysis of Hump Formation Mechanism in Double-Suction Centrifugal Pump under Part Load Condition

open access: yesEnergies, 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
doaj   +1 more source

A new stall-onset criterion for low speed dynamic-stall [PDF]

open access: yes, 2005
The Beddoes/Leishman dynamic-stall model has become one of the most popular for the provision of unsteady aerofoil data embedded in much larger codes.
Beddoes   +20 more
core   +1 more source

Propagation of stall in a compressor blade row [PDF]

open access: yes, 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.
core   +1 more source

Delaying the Stall of A Low-Wing Aircraft Using A Novel Powerful Vortex Generator

open access: yesInventions, 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
doaj   +1 more source

Boundary Layer Separation and Reattachment Detection on Airfoils by Thermal Flow Sensors

open access: yesSensors, 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
doaj   +1 more source

Detection and Analysis of an Alternate Flow Pattern in a Radial Vaned Diffuser

open access: yesInternational 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
doaj   +1 more source

Determination of Ranges of Unstable Operation of Axial Compressor for Aircraft Turbine Engines [PDF]

open access: yesProblemy 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
doaj   +1 more source

Aerodynamic Characteristics of Different Airfoils under Varied Turbulence Intensities at Low Reynolds Numbers

open access: yesApplied 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
doaj   +1 more source

Flow Behavior Caused by Air Permeability of Ski Jumping Suit Fabric

open access: yesProceedings, 2020
The purpose of this study was to investigate the effect of the air permeability of ski jumping suit fabric on aerodynamic characteristics. In the study, four types of fabric with different air permeabilities were installed onto a fabric-clothed elliptic ...
Yuki Kataoka   +4 more
doaj   +1 more source

Evolution Characteristics of Separated Vortices and Near-Wall Flow in a Centrifugal Impeller in an Off-Designed Condition

open access: yesApplied Sciences, 2020
Flow separation is undesirable and lowers the efficiency of centrifugal impellers. In this study, the evolution characteristics of separated vortices in a centrifugal impeller are studied under the off-designed flow rate condition.
Shihao Zhou   +3 more
doaj   +1 more source

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