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Advances in Unsteady Turbomachinery Aerodynamics in Japan: Professor Gallus’ Contribution

[+] Author Affiliations
Toshinori Watanabe, Hideo Tanaka

University of Tokyo, Tokyo, Japan

Eisuke Outa

Waseda University, Tokyo, Japan

Tsutomu Adachi

University of Tsukuba, Tsukuba, Japan

Ichiro Ariga

Keio University, Yokohama, Japan

Yasushige Kashiwabara

Kanagawa Institute of Technology, Kanagawa, Japan

Shimpei Mizuki

Hosei University, Tokyo, Japan

Paper No. GT2005-68695, pp. 39-50; 12 pages
doi:10.1115/GT2005-68695
From:
  • ASME Turbo Expo 2005: Power for Land, Sea, and Air
  • Volume 6: Turbo Expo 2005, Parts A and B
  • Reno, Nevada, USA, June 6–9, 2005
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-4730-6 | eISBN: 0-7918-3754-8
  • Copyright © 2005 by ASME

abstract

The present paper describes recent advances in turbomachinery aerodynamic research in Japan achieved by the researchers who studied under the supervision of the late Professor Gallus. His research work, way of thinking, and personality exerted great influence in Japan on the styles of research in the field of unsteady aerodynamics of turbomachines. The profound contribution by him to the research and development of Japanese gas turbine technologies is highly appreciated. The paper presents research results on the issues concerning cascade flutter suppression, rotating stall analysis and control for axial compressors, unsteady flow analysis and control for radial compressors and diffusers, as well as design studies of axial turbomachines.

Copyright © 2005 by ASME

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