Results 271 to 280 of about 34,550 (312)
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Unsteady Flow in Axial Flow Compressors
1991A review is made of the experimental rotating stall work on a low-speed compressor stage. The instantaneous flow field inside the cell is explored using multiple hot wires in the absolute frame of reference. Rotor blade stall and radial drift of the boundary layer is investigated by on-rotor blade instrumentation.
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A Study of the Supersonic Axial-Flow Compressor
Journal of Applied Mechanics, 1949Abstract This paper presents a summary of the basic principles of the supersonic compressor and an analytical study of the types of this compressor most likely to prove successful. This study assumes rather idealized conditions, ignoring such variables as radial effects and flow irregularities.
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Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 1999
The purpose of this paper is to set out some of the basic principles and rules associated with the design of axial flow compressors, principally for aero-engines, as well as the practical constraints that are inevitably present. The thrust is primarily on the aerodynamic design but this cannot be divorced from the mechanical aspects and so some of ...
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The purpose of this paper is to set out some of the basic principles and rules associated with the design of axial flow compressors, principally for aero-engines, as well as the practical constraints that are inevitably present. The thrust is primarily on the aerodynamic design but this cannot be divorced from the mechanical aspects and so some of ...
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An Improved Axial Flow Compressor Design
The Journal of the Royal Aeronautical Society, 1965In using the method of stage stacking to compute the off-design performance of multi-stage axial compressors, it has been observed that the limitation on performance at speeds above the design speed has been set by the stall and the choke points of the rear stages(1).
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Bifurcation Analysis of Axial Flow Compressor Stability
SIAM Journal on Applied Mathematics, 1990With a one-mode truncation it is possible to reduce the Moore–Greitzer model for compressor instability to a set of three ordinary differential equations. These are approached from the point of view of bifurcation theory. Most of the bifurcations emerge from a degenerate Takens–Bogdanov bifurcation point.
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Mathematical modelling and design of the ionic liquid compressor for the hydrogen refuelling station
International Journal of Energy Research, 2022Xueyuan Peng
exaly
Axial Flow Compressor Noise Studies
SAE Technical Paper Series, 1962T. G. Sofrin, J. M. Tyler
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Flow characteristics of tangential leakage in a scroll compressor for automobile heat pump with CO2
Science China Technological Sciences, 2021Mingshan Wei, Chenxing Hu
exaly