Results 11 to 20 of about 176,725 (228)
Volume 2: Automotive Systems, Bioengineering and Biomedical Technology, Fluids Engineering, Maintenance Engineering and Non-Destructive Evaluation, and Nanotechnology, 2006 A global methodology has been developed and validated to obtain the total pressure loss coefficient in internal compressible flow at T-type junctions. This methodology is based on the calculation of the thermo-fluid properties extrapolated to the branch axes intersection, once the straight pipe friction losses numerically calculated have been ...
Pérez García, José +3 more
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Preliminary Experimental Study on Pressure Loss Coefficients of Exhaust Manifold Junction
International Journal of Rotating Machinery, 2014 The flow characteristic of exhaust system has an important impact on inlet boundary of the turbine. In this paper, high speed flow in a diesel exhaust manifold junction was tested and simulated.
Xiao-lu Lu +4 more
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Performance Optimization of the Helical Heat Exchanger With Turbulator
Frontiers in Energy Research, 2022 In this paper, optimization on a two-tube helical heat exchanger with a fin is represented. The spiral pipes heat exchanger which is made of the cooper is adopted for investigation. The effects of three types of fins with the proposed geometric shapes on
Wang Xifeng +6 more
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VIGV Angle Optimization for Subsonic Axial Flow Compressor [PDF]
INCAS Bulletin, 2020 Long-term performance of an axial-flow compressor by the scheduling of inlet guide vanes at off-design conditions has been studied in this paper. The compressors are used in various industries and in aviation sectors for different operations at different
Prabhat SINGH, Dharmahinder Singh CHAND
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Prediction of secondary flow losses in an entrance duct to a low-pressure turbine
Archives of Mechanics, 2019 Secondary flow features and total pressure losses by means of the total pressure loss coefficient are discussed in an entrance duct, named a turbine central frame (TCF), to a four-stage low-pressure turbine (LPT) of aero-engine.
P. Jonak, T. Borzęcki, S. Kubacki
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Effects of Configuration and Slot Angle of the Bleed System on the Performance of Hypersonic Inlet
气体物理, 2023 The numerical simulation of a typical two-dimensional hypersonic inlet was carried out to study the effects of configuration and slot angle of the bleed system on the performance of hypersonic inlet.
Hao-Yu CHEN, He-Xia HUANG, Hui-Jun TAN
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AERODYNAMIC STUDIES IN THE STATIC COMPONENTS OF A CENTRIFUGAL COMPRESSOR STAGE [PDF]
Journal of Mechanical Engineering and Sciences, 2011 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 0.053
K. Srinivasa Reddy +2 more
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Comparative Study on the Performance of S-Shaped Diffuser With Shorten Length
MATEC Web of Conferences, 2018 This study presents numerical investigation on the performance of S-shaped air intake normal and aggressive diffuser with 22% length reduction. Both models have same area ratio of 3.1 with different total length, turning angle and radius of curvature ...
Jessam Raed A. +2 more
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Iterative calculation of local head loss coefficient of emitters in lateral lines [PDF]
Revista Brasileira de Engenharia Agrícola e AmbientalThis study aimed to iteratively set the local head loss coefficient of the Naan® micro-sprinkler, model 7110 Hadar, installed in a lateral irrigation line.
Giuliani Prado +4 more
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Numerical study on variable area afterburner with wide bypass ratio
Xibei Gongye Daxue XuebaoTo investigate the impact of variable geometry components on the performance of afterburner, the afterburner of triangular variable connotation components was designed, and the effects of the different state points and duct ratio on the total pressure ...
Ma Yinzhang +3 more
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