Results 1 to 10 of about 4,068 (307)

VIGV Angle Optimization for Subsonic Axial Flow Compressor [PDF]

open access: diamondINCAS 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
doaj   +2 more sources

The New Performance Calculation Method of Fouled Axial Flow Compressor [PDF]

open access: yesThe Scientific World Journal, 2014
Fouling is the most important performance degradation factor, so it is necessary to accurately predict the effect of fouling on engine performance. In the previous research, it is very difficult to accurately model the fouled axial flow compressor.
Huadong Yang, Hong Xu
doaj   +2 more sources

Axial-flow compressor analysis under distorted phenomena at transonic flow conditions

open access: goldCogent Engineering, 2018
Today, the turbomachinery engineering plays a vital role in the field of air breathing propulsion, most importantly the components like compressor, turbine and its possible numerical strategies to improve the overall efficiency especially in the ...
G Srinivas   +2 more
doaj   +2 more sources

Experimental Investigation of Rotor-Stator Interaction in Axial-Flow Turbines and Compressors [PDF]

open access: goldInternational Journal of Rotating Machinery, 1998
Detailed results of unsteady flow measurements in a stator-rotor-stator assembly of an axial-flow turbine as well as an inlet guide vane-rotor-stator formation of an axial-flow compressor are presented in this paper.
Heinz E. Gallus
doaj   +2 more sources

FLOW SEPARATION OF AXIAL COMPRESSOR CASCADE BLADES

open access: goldJournal of Engineering, 2010
An experimental and theoretical investigation of the effect of flow separation on the performance of a cascade NACA 65_(12)10 axial compressor blade has been carried out.
Arkan Kh. Al-Taie, Sabah Faleh Habeeb
doaj   +5 more sources

The investigation of absolute flow non-uniform velocity distributions influence at the centrifugal compressor axial radial impeller inlet using numerical calculation methods in ANSYS CFX [PDF]

open access: diamondE3S Web of Conferences, 2019
Currently, methods of numerical modelling are widely used. They are especially widely used in the design of turbo compressors. For the specific task of designing new flowing parts of a centrifugal compressor, it is not recommended to deviate from the ...
Rakhmanina L.A.   +4 more
doaj   +2 more sources

A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors [PDF]

open access: yesFundamental Research
The air intake-compression systems of modern aircraft usually use the aero-engine intake and fan/compressor as the main components. Inlet-engine compatibility has always been the key to the stable and safe operation of the propulsion system, including ...
Zhenyu Li   +3 more
doaj   +2 more sources

Numerical Study on End Wall Synthetic Jet to Improve Performance and Stability Margin of a High-speed Subsonic Axial Compressor Rotor [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2023
Synthetic jet has been confirmed as a novel flow control technology. However, the existing application research on synthetic jet in axial flow compressor is still confined to cascade or low-speed axial flow compressors, and rarely high-speed axial flow ...
G. Wang, W. Chu, W. Liu
doaj   +1 more source

Impact Investigation of Stator Seal Leakage on Aerodynamic Performance of Multistage Compressor

open access: yesFrontiers in Energy Research, 2021
In this paper, a numerical model based on the mass flow rate of seal leakage is presented, and a 3D numerical method of a multistage axial compressor with good engineering practicability is established.
Qi Wang   +7 more
doaj   +1 more source

Test problem of flow modelling in the Rotor 37 compressor stage

open access: yesАвіаційно-космічна техніка та технологія, 2023
The subject of the study is the dependence of the degree of pressure increase on the airflow in the impeller of the axial compressor degree. The object of study is the Rotor 37 axial compressor.
Andrii Duliepov   +4 more
doaj   +1 more source

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