MULTISTAGE AXIAL COMPRESSOR MAP GENERATION
Abstract
A one-dimensional theory regarding the change of state in a multistage axial compressor at design point and part load has been formulated. With regard to short calculation times for obtaining compressor maps this algorithm is suitable to get insight into the main parameters influencing the off-design behaviour. An 'academic' test example, representing a 3-stage subsonic compressor, has been used for tests.
Keywords:
axial compressor, thermodynamic, computation methodHow to Cite
KÓBOR, Ágota “MULTISTAGE AXIAL COMPRESSOR MAP GENERATION”, Periodica Polytechnica Mechanical Engineering, 37(2), pp. 111–131, 1993.
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