Calculation of Compressible Subsonic Flow in Cascades With Varying Blade HeightSource: Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 004::page 345Author:R. A. Van den Braembussche
DOI: 10.1115/1.3445742Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper deals with a singularity method to calculate the subsonic compressible flow in compressor and turbine cascades, with constant or varying blade height. The method is an extension of an incompressible flow method by means of the Janzen-Rayleigh theorem, using an exact relation between pressure and density. Theoretical results are compared with experimental data. A further extension of this method to rotational flow in plane cascades obtained from the transformation of the blade to blade surface of a mixed flow machine is also discussed.
keyword(s): Blades , Subsonic flow , Flow (Dynamics) , Machinery , Compressors , Turbines , Compressible flow , Rotational flow , Theorems (Mathematics) , Density AND Pressure ,
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| contributor author | R. A. Van den Braembussche | |
| date accessioned | 2017-05-09T01:36:21Z | |
| date available | 2017-05-09T01:36:21Z | |
| date copyright | October, 1973 | |
| date issued | 1973 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-25381#345_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/163753 | |
| description abstract | This paper deals with a singularity method to calculate the subsonic compressible flow in compressor and turbine cascades, with constant or varying blade height. The method is an extension of an incompressible flow method by means of the Janzen-Rayleigh theorem, using an exact relation between pressure and density. Theoretical results are compared with experimental data. A further extension of this method to rotational flow in plane cascades obtained from the transformation of the blade to blade surface of a mixed flow machine is also discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Calculation of Compressible Subsonic Flow in Cascades With Varying Blade Height | |
| type | Journal Paper | |
| journal volume | 95 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3445742 | |
| journal fristpage | 345 | |
| journal lastpage | 351 | |
| identifier eissn | 0742-4795 | |
| keywords | Blades | |
| keywords | Subsonic flow | |
| keywords | Flow (Dynamics) | |
| keywords | Machinery | |
| keywords | Compressors | |
| keywords | Turbines | |
| keywords | Compressible flow | |
| keywords | Rotational flow | |
| keywords | Theorems (Mathematics) | |
| keywords | Density AND Pressure | |
| tree | Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 004 | |
| contenttype | Fulltext |