A 2D aerodynamic design of subsonic axial compressor stage
نویسندگان
چکیده
منابع مشابه
Design and simulation of flow through subsonic axial compressor
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~ blade-element theory for aanid--ow compre8sor8has been deoeloped and applied to the anulysi8 of the. effects of basic deeign variabkwvuch as Mach number, blude loading, and mJocily didn”buiion on compree80r performance. A graphi.cul method tlwt ia u8efulfor approximate design cakulati0n8 i8 pre8ented. Tle relati0n8 among 8e8eralefinci48 useful in compressor design are derived and &cu8sed. The...
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the purpose of this study is to design a three-stage axial compressor with identical pressure ratio which makes an adequate pressure ratio and efficiency in design point conditions with rotational velocity of 38000rpm and mass flow rate of 3.2kg/s. first of all, considering some restrictions such as dehaller number more than 0.7 in all sections of the stator and the rotor, and relative mach num...
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ژورنال
عنوان ژورنال: Fluid Mechanics research International Journal
سال: 2018
ISSN: 2577-8242
DOI: 10.15406/fmrij.2018.02.00030