Analysis of aerodynamic performance of high‐speed rotational components for MEMS based turbomachinery considering effects of tip clearance and diabatic heat transfer

This paper addresses a fundamental design guideline for rotational components of a micro‐scale gas turbine engine considering an interaction between geometrical structure and aerodynamics. The rotational components of the micro‐scale gas turbine engine may be subjected to the centrifugal stress due...

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Veröffentlicht in:	Electronics and communications in Japan 2021-12, Vol.104 (4), p.n/a
Hauptverfasser:	Tanaka, Shuusei, Nakai, Takaaki, Toriyama, Toshiyuki
Format:	Artikel
Sprache:	eng
Schlagworte:	adiabatic efficiency Aerospace engines Centrifugal compressors compressor Compressor efficiency Elastic deformation Gas turbine engines Heat transfer MEMS Tip clearance turbine Turbomachinery
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