Analysis of Aerodynamic Performance of a Microscale Radial Flow Wave-rotor for Gas Turbine Topping Cycle-Reference-Cited by-同舟云学术

Analysis of Aerodynamic Performance of a Microscale Radial Flow Wave-rotor for Gas Turbine Topping Cycle

Published:2019-08-01 Issue:8 Volume:139 Page:225-237
ISSN:1341-8939
Container-title:IEEJ Transactions on Sensors and Micromachines
language:en
Short-container-title:IEEJ Trans. SM

Author:

Taguchi Shori¹,Rikuno Kohei¹,Kumagai Shinya¹,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/139/8/139_225/_pdf

Reference17 articles.

1. (1) H. Sumi, K. Rikuno, R. Suzuki, and T. Toriyama : “Analysis of Aerodynamic Components Matching for Microscale Gas Turbine Engine”, IEEJ Trans. SM, Vol. 138, No. 4, pp. 132-144 (2018) (in Japanese)

2. (2) F. Iancu, P. Akbari, and N. Muller : “Feasibility Study of Integrating Four-Port Wave Rotor into Ultra-Micro Gas Turbines(UµGT)”, 40th AiAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, USA (2004)

3. (3) H. E. Weber : Shock Wave Engine Design, p. 56, John Wiley & Sons (1994)

4. (4) D. E. Paxson: “A General Numerical Model for Wave Rotor Analysis”, NASA Technical Memorandum 105740 (1992)

5. (5) G. E. Welch, S. M. Jones, and D. E. Paxson : “Wave Rotor-Enhanced Gas Turbine Engines”, NASA Technical Memorandum 106998 (1993)

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