Results 41 to 50 of about 33,160 (211)
Wake Mixing in Axial Flow Compressors [PDF]
Over the years it has been speculated that the performance of multi-stage axial flow compressors is enhanced by the passage of a wake through a blade row prior to being mixed-out by viscous diffusion. The link between wake mixing and performance depends on the ability to recover the total pressure deficit of a wake by a reversible flow process.
openaire +1 more source
Experimental Investigation of the Flow Field in a Multistage Axial Flow Compressor
The nature of the flow field in a three stage axial flow compressor, including a detailed survey at the exit of an embedded stator as well as the overall performance of the compressor is presented and interpreted in this paper.
B. Lakshminarayana +3 more
doaj +1 more source
Experimental study of endwall flow in a low-speed linear compressor cascade: effect of over-tip leakage [PDF]
This paper describes the study of endwall flow modification due to over-tip leakage flow in axial compressor blades. Un-shrouded axial compressor stator and rotor blades in aero-engines and land based gas turbines are subjected to over-tip leakage flow ...
Kanjirakkad, Vasudevan
core +1 more source
In order to investigate the effect of a synthetic jet arranged at the suction surface on the aerodynamic performance of an axial flow compressor, a high-speed subsonic axial flow compressor rotor was numerically simulated in this paper.
Guang Wang +3 more
doaj +1 more source
Flow measurements in the discharge port of a screw compressor [PDF]
The angle-resolved mean velocity and turbulence characteristics of axial air flow within the rotors and discharge chambers of a screw compressor have been measured, using a laser Doppler velocimeter with high spatial and temporal resolution.
C Arcoumanis +6 more
core +1 more source
Effect of Blade Slot Positioning Close to Blade Root on the Performance of Highly Loaded Helium Compressor [PDF]
The helium compressor has the inherent characteristics of a lower single-stage pressure ratio and a higher number of stages than an air compressor. The highly loaded design method effectively addressed the compressibility issue of the helium compressor ...
Y. Fan +4 more
doaj +1 more source
A turbojet simulator for Mach numbers up to 2.0 [PDF]
A turbojet simulator was designed and fabricated for use in wind tunnel models. The simulator contains a six-stage, axial-flow compressor powered by a three-stage, axial-flow turbine. High pressure heated air was used to drive the turbine.
Nosek, S. M. +3 more
core +1 more source
CFD investigation of transonic axial compressor rotor blade at various off-design conditions [PDF]
Flow separation over blade surfaces is an important parameter and its reduction or elimination can improve better aerodynamic performance, efficiency and stall margin.
Ahmad, Kamarul Arifin +2 more
core
FLOW SEPARATION OF AXIAL COMPRESSOR CASCADE BLADES
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 +3 more sources
Oscillatory Tip Leakage Flows and Stability Enhancement in Axial Compressors
Rotating stall axial compressor is a difficult research field full of controversy. Over the recent decades, the unsteady tip leakage flows had been discovered and confirmed by several research groups independently.
Feng Lin, Jingyi Chen
doaj +1 more source

