Numerical Simulation of a Mixed-flow Compressor under Windmill Conditions-Reference-Cited by-同舟云学术

Numerical Simulation of a Mixed-flow Compressor under Windmill Conditions

Published:2015 Issue:0 Volume:13 Page:1-10
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

NOJI Yuya¹,ICHIMURA Jun¹,MORIYAMA Masayuki¹,SATO Tetsuya¹,MASAKI Daisaku²,TAGUCHI Hideyuki²

Affiliation:

1. Mechanical Science Faculty of Fundamental, Science and Engineering, Waseda University

2. Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/13/0/13_TJSAS-D-13-00007/_pdf

Reference14 articles.

1. 1) Kobayashi, H.: Windmill Starting Characteristics of Core Engine for Hypersonic Aircraft, Proceedings of Space Transportation Symposium, Tokyo, Japan, 2009 (in Japanese).

2. 2) Prasad, D., and Lord, W. K.: Internal Losses and Flow Behavior of a Turbofan Stage at Windmill, Journal of Turbomachinery, 132 (2010), 031007.

3. 3) Gill, A., von Backstrom, T.W., and Harms, T. M.: The Flow Field within an Axial Flow Compressor at Extremely High Flow Coefficients, Proceedings of ASME Turbo Expo 2010, Glasgow, UK, GT2010-22894, 2010.

4. 4) Imaeda, M., Kato, D., Ohta, Y., Totani, D., and Outa, E.: Detail Flow Field Investigation of an Axial Flow Compressor at Windmill Conditions, Proceedings of International Gas Turbine Congress 2011 Osaka, Osaka, Japan, GT2011-0030, 2011.

5. 5) Jen, P. C., Amrit, R. G., Kidambi, S., and David, L. W.: Comparison of Computations Using Navier-Stokes Equations in Rotating and Fixed Coordinates for Flow through Turbomachinery, AIAA Paper 97, 1997.