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Solidity and camber angle are key parameters with a primary effect on airfoil diffusion. Maximum thickness location has a considerable impact on blade loading distribution. This paper investigates correlations of maximum thickness location, solidity, and
Chuansijia Tao +5 more
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Aerodynamic Studies in the Static Components of A Centrifugal Compressor Stage Authors [PDF]
Aerodynamic studies in the static components of a centrifugal compressor stage were conducted using the computational fluid dynamics solver FLUENT. For the simulation study, a typical centrifugal compressor stage geometry with a flow coefficient of 0 ...
K. Srinivasa Reddy +2 more
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In this paper, the measurement accuracy of two different types of total pressure probe and total temperature probe in turboshaft engine compressor inlet channel and the influence of these two probes on the flow field through numerical simulation was ...
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Investigation of the Effects of Different Working Fluids on Compressor Cascade Performance
The compressor of closed Brayton cycle (CBC) plant operating with working fluid other than air is a vital element of the energy conversion unit. However, due to insufficient understanding of the influence of the physical properties of working fluids on ...
Zhitao Tian, Chengze Wang, Qun Zheng
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Effect of inlet and outlet angles on the flow performance of the ferrofluidic magnetic micropump
The paper presents a CFD investigation of the effect of the inlet and outlet angles on the flow performance of the ferrolfuidic magnetic mircropump. The methodology employed is based on treating the overall flow path in the inlet or outlet chambers as a ...
Sufian Shaker +3 more
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Flow performance comparison along the centerline in straight and s shaped diffuser
In this paper of the S shaped diffuser with area ratio (AR) 1.5, an experimental investigation was conducted to a nalyze the effect of the change in curvature of a straight wall diffuser.
Hardial SİNGH
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ObjectivesIn order to improve the working performance of gas turbines, this study examines the aerodynamic performance of variable geometry turbine clamshell guide vanes.MethodsTaking a typical variable geometry turbine guide vane as a prototype, a ...
Tao TANG +3 more
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The jet always sweeps to the leftmost and rightmost points in the sweeping jet and film composite cooling (SJF) process, resulting in a different coolant flow in each film hole. The film can not easily cover the outer surface evenly under the scouring of
Xiangcan Kong +5 more
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The four-duct-annular advanced vortex combustor(AVC)has small duct area near the combustor axis of cooling burn wall and middle two-duct, which can be served as duty fire duct under poor oil burning.The numerical simulation is carried out by considering ...
ZHANG Changtian, LIU Jingyuan
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Various sensors are used in the aero-engine during the test, and the probe as a contact measurement tool is bound to change the internal flow state of the flow field and affect the measurement accuracy.
ZHENG Guanghua +4 more
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