Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 3 - Performance of blowing insert configuration no. 1 [PDF]
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and performance tests using distorted or undistorted inlet ...
Koch, C. C., Smith, L. H., Jr.
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Computational fluid dynamics simulations of blade damage effect on the performance of a transonic axial compressor near stall [PDF]
, 2014 Gas turbine axial compressor blades may encounter damage during service for various reasons such as damage by debris from casing or foreign objects impacting the blades, typically near the rotor’s tip.
Abdulnaser I Sayma +4 more
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Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor [PDF]
Overall stage and stator blade element performance with straight stator and tilted stator in transonic axial flow compressor ...
Cullom, R. R. +2 more
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Учет неосесимметричности течения в осевых турбомашинах [PDF]
, 2008 The approach under the account of the defective phenomena is observed by development of mathematical models of current in meridional plane of axial turbomachines.
Ковалева, Е. А. +3 more
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Effect of Various Blade Modifications on Performance of A16-Stage Axial-Flow Compressor. V - Effect on Over-All Performance Characteristics of a 20-Percent Reduction in Solidity of the Fourteenth Through Sixteenth Stage Rotors [PDF]
, 1952 The performance of a 16-stage axial-flow compressor, in which the mean-radius solidity was reduced from 1.28 to 1.02 in the fourteenth through sixteenth stage rotors was determined.
Hatch, James E., Medeiros, Arthur A.
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Effects of inlet treatment location and treatment cavity depth on compressor noise [PDF]
The ability of acoustic liners to reduce compressor noise inside and in front of an inlet was studied. An axial flow research compressor and a specially designed inlet were used inside an anechoic chamber.
Clark, L. R.
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Simulation of Casing Treatments of a Transonic Compressor Stage
International Journal of Rotating Machinery, 2008 This article presents the study of casing treatments on an axial compressor stage for improving stability and enhancing stall margin. So far, many simulations of casing treatments on single rotor or rotor-stator configurations were performed.
M. Hembera, H.-P. Kau, E. Johann
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High-speed laser anemometer system for intrarotor flow mapping in turbomachinery [PDF]
A fringe-type laser anemometer with innovative features is described. The innovative features include: (1) rapid, efficient data acquisition processes, (2) detailed graphic display of data being accumulated, and (3) input laser-beam positioning that ...
Powell, J. A. +2 more
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Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines [PDF]
, 1947 Investigations were conducted in the Cleveland altitude wind tunnel to determine the performance and operational characteristics of the 19B-2, 19B-8, and 19XS-1 turbojet engines.
Dietz, Robert O., Kuenzig, John K.
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Blade selection for a modern axial-flow compressor [PDF]
The procedures leading to successful design of an axial flow compressor are discussed. The three related approaches to cascade selection are: (1) experimental approach which relies on the use of experimental results from identical cascades to satisfy the
Wright, L. C.
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