Results 251 to 260 of about 7,604 (310)
Axial Compressor Design with Counter-Rotation and Variable RPM for Stall Mitigation
, 2014 Madhur Tiwari
openalex +1 more source
Development and Application of a Laboratory Simulation Device for the Underground Compressed Air Energy Storage System. [PDF]
ACS OmegaFu Y, Chen S, Zheng K, Zhang Y.
europepmc +1 more source
Cylinder-piston application for surge prevention and energy efficiency in an industrial compression unit. [PDF]
HeliyonGhanbari A, Mazaheri K.
europepmc +1 more source
Some of the next articles are maybe not open access.
Related searches:
Related searches:
Axial Compressor Stator Aerodynamics
Journal of Engineering for Gas Turbines and Power, 1985Axisymmetric, through-flow calculations, currently the “backbone” of most multistage turbomachinery design systems, are being pushed to their limit. This is due to the difference between the complex, three-dimensional flows that actually occur in turbomachinery and the two-dimensional flow assumed in this type of analysis.
H. D. Joslyn, R. P. Dring
openaire +1 more source
Aeronautical Quarterly, 1949
It is fairly generally known that if, at any fixed speed of a compressor, either axial or centrifugal, the flow is reduced by throttling the outlet, then a point is eventually reached at which a complete breakdown of the air flow occurs and in most cases an actual flow reversal through the compressor takes place.
H. Pearson, T. Bowmer
openaire +1 more source
It is fairly generally known that if, at any fixed speed of a compressor, either axial or centrifugal, the flow is reduced by throttling the outlet, then a point is eventually reached at which a complete breakdown of the air flow occurs and in most cases an actual flow reversal through the compressor takes place.
H. Pearson, T. Bowmer
openaire +1 more source
The Journal of the Royal Aeronautical Society, 1959
The note in the July Journal by H. Pearson and A. B. McKenzie (p. 415) shows that the flow into an axial compressor is nearly at a constant velocity at all points in the entry plane; and that if a wake of low energy air is fed into it, the compressor reduces the static pressure locally in this wake, in such a way as to tend to preserve constant ...
H. Pearson, A. B. McKenzie
openaire +2 more sources
The note in the July Journal by H. Pearson and A. B. McKenzie (p. 415) shows that the flow into an axial compressor is nearly at a constant velocity at all points in the entry plane; and that if a wake of low energy air is fed into it, the compressor reduces the static pressure locally in this wake, in such a way as to tend to preserve constant ...
H. Pearson, A. B. McKenzie
openaire +2 more sources
Axial Compressor Performance Maintenance
Volume 4: Turbo Expo 2005, 2005Methods of compressor performance maintenance for large utility combustion turbines continue to evolve. On-line water wash systems used to recover performance loss due to fouling are evolving that use less water. This paper derives a water wash model based on a thin film of water covering the airfoil surfaces.
Philip Levine, Leonard Angello
openaire +1 more source
1979
The only additional material here over that in chapter 4 is that it is convenient in the velocity diagrams to specify angles δ and γ for trigonometric purposes and polytropic stage efficiency is of importance since axial compressors, which are usually multistage machines are mostly designed on the basis of one stage with an assumed constant stage ...
openaire +1 more source
The only additional material here over that in chapter 4 is that it is convenient in the velocity diagrams to specify angles δ and γ for trigonometric purposes and polytropic stage efficiency is of importance since axial compressors, which are usually multistage machines are mostly designed on the basis of one stage with an assumed constant stage ...
openaire +1 more source
The Journal of the Royal Aeronautical Society, 1959
A centrifugal compressor rotor is quite robust, but the blading of an axial compressor looks horrifyingly fragile and very susceptible to damage by objects sucked into the engine. The introduction of axial compressor engines into airline service brings this again to the attention of designers and service engineers.
openaire +2 more sources
A centrifugal compressor rotor is quite robust, but the blading of an axial compressor looks horrifyingly fragile and very susceptible to damage by objects sucked into the engine. The introduction of axial compressor engines into airline service brings this again to the attention of designers and service engineers.
openaire +2 more sources
Rotating Stall in Axial Flow Compressors
Journal of the Aeronautical Sciences, 1957The classical theories of linearized aerodynamics yields a complete description of the flow field due to the rotating stall in a two-dimensional cascade of airfoils, when the extension of the stalled region is small. The corresponding physical scheme can be used for larger stalled regions, without the limitations of the linearizing assumptions, if no ...
Fabri, Jean, Siestrunck, Raymond
openaire +2 more sources