Analysis of Aerodynamic Performance of High-Speed Rotational Components for MEMS Based Turbomachinery Considering Effects of Tip Clearance and Diabatic Heat Transfer-Reference-Cited by-同舟云学术

Analysis of Aerodynamic Performance of High-Speed Rotational Components for MEMS Based Turbomachinery Considering Effects of Tip Clearance and Diabatic Heat Transfer

Published:2021-06-01 Issue:6 Volume:141 Page:164-172
ISSN:1341-8939
Container-title:IEEJ Transactions on Sensors and Micromachines
language:en
Short-container-title:IEEJ Trans. SM

Author:

Tanaka Shuusei¹,Nakai Takaaki¹,Toriyama Toshiyuki¹

Affiliation:

1. College of Science and Engineering, Ritsumeikan University

Publisher

Institute of Electrical Engineers of Japan (IEE Japan)

Subject

Electrical and Electronic Engineering,Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/ieejsmas/141/6/141_164/_pdf

Reference9 articles.

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2. 角宙樹・陸野晃平・鈴木涼馬・鳥山寿之：「マイクロスケールガスタービン用空力要素のマッチング解析」, 電学論E, Vol. 138, No. 4, pp. 132-144 (2018)

3. (2) B. Sirakov, Y. Gong, A. Epstain, and C. Tan : “DESIGN AND CHARACTERIZATION OF MICROCOMPRESSOR IMPELLERS”, ASME Turbo Expo 2004, Vol. 5, No. GT2004-53332, pp. 737-746 (2004)

4. (3) Y. Gong, B. Sirakov, A. Epstain, and C. Tan : “AEROTHERMODYNAMICS OF MICROTURBOMACHINERY”, ASME Turbo Expo 2004, Vol. 6, No. GT2004-53877, pp. 95-102 (2004)

5. (4) H. I. H. Saravanamuttoo, G. F. C. Rogers, H. Cohen, and P. V. Straznicky (著), 藤原仁志 (訳)：「ガスタービンの基礎と応用発電用からジェットエンジンまで」, 東海大学出版社 (2012)

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