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Of the compressor disc using Sagerser Empirical Weight Estimation. Geometrical parameters, velocity triangle, and weight and stress calculations Techniques employed the basic thermodynamic and aerodynamic theory of axialįlow compressors to determine the temperature and pressure for all stages, Furthermore, in order to evaluate the conceptual design analysis,īasic parameters like compressor sizing, load and blade mass, disc stressĪnalysis, bearings and material selections, conceptual disc design and rotorĭynamics are considered using existing tools and analytical technique. IND100 with an overall pressure ratio of 12 and mass flow of 310 kg/s at ISOSLSĬonditions. This paper presents the structural andĬonceptual design of a sixteen stage single shaft high pressure compressor of Sometimes act in opposition, hence engineering balance is employed within the Structural integrity analysis of the component. Interrelationship between the thermodynamic, aerodynamic, mechanical design and Structural design of the IND100 axial compressor requires a multistage
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