Experimental Investigation of Unsteady Pressure on an Axial Compressor Rotor Blade Surface
نویسندگان
چکیده
منابع مشابه
Numerical Investigation of Single Stage of an Axial Flow Compressor for Effects of Blade Aspect Ratio
In present work, a compressor configuration is taken from literature which will be studied for aspect ratio (ratio between length of blade to chord length) influence over performance. Performance in the sense is pressure ratio of compressor. The aspect ratio of the blade is an important parameter and has a strong influence on the performance of axial flow compressor. There are so many literatur...
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Introduction. This paper deals with some transonic flow problems for the supersonic axial flow compressor: these arise in connection with flutter analysis for fan blading. Very detailed solutions for unsteady plane transonic flows through a cascade of flat plates have been given by Goldstein Braun and Adamczyk (1977) and Nagashima and Whitehead (1977), see also Goldstein (1975), Kurosaka (1974)...
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ژورنال
عنوان ژورنال: Energy and Power Engineering
سال: 2010
ISSN: 1949-243X,1947-3818
DOI: 10.4236/epe.2010.22019