Some Investigations Into Transonic Axial-Flow Compressors With High Stage Load Coefficients and Low Degrees of ReactionSource: Journal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 003::page 286Author:Karl E. Wichert
DOI: 10.1115/1.3673189Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A design for a transonic axial-flow compressor is described, in which a rotor wheel with a low degree of reaction operates in subsonic flow and the stator operates in supersonic flow. A compressor was run as a single-stage compressor and an outlet pressure ratio equal to that of an orthodox compressor with 4 stages. Some discussion of another compressor in which both the rotor wheel and the stator operate in supersonic flow is also given.
keyword(s): Compressors , Stress , Axial flow , Stators , Supersonic flow , Wheels , Rotors , Pressure , Design AND Subsonic flow ,
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| contributor author | Karl E. Wichert | |
| date accessioned | 2017-05-09T01:08:02Z | |
| date available | 2017-05-09T01:08:02Z | |
| date copyright | July, 1961 | |
| date issued | 1961 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26617#286_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/154834 | |
| description abstract | A design for a transonic axial-flow compressor is described, in which a rotor wheel with a low degree of reaction operates in subsonic flow and the stator operates in supersonic flow. A compressor was run as a single-stage compressor and an outlet pressure ratio equal to that of an orthodox compressor with 4 stages. Some discussion of another compressor in which both the rotor wheel and the stator operate in supersonic flow is also given. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Some Investigations Into Transonic Axial-Flow Compressors With High Stage Load Coefficients and Low Degrees of Reaction | |
| type | Journal Paper | |
| journal volume | 83 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3673189 | |
| journal fristpage | 286 | |
| journal lastpage | 290 | |
| identifier eissn | 0742-4795 | |
| keywords | Compressors | |
| keywords | Stress | |
| keywords | Axial flow | |
| keywords | Stators | |
| keywords | Supersonic flow | |
| keywords | Wheels | |
| keywords | Rotors | |
| keywords | Pressure | |
| keywords | Design AND Subsonic flow | |
| tree | Journal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 003 | |
| contenttype | Fulltext |