Effects of Low Reynolds Number on Performance in a Centrifugal Compressor-Reference-Cited by-同舟云学术

Effects of Low Reynolds Number on Performance in a Centrifugal Compressor

Published:2018 Issue:6 Volume:61 Page:238-247
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

KIM Jaehyo¹,JEON Heungsu¹,JUNG Yohan²,PARK Jun Young³,CHOI Minsuk¹

Affiliation:

1. Department of Mechanical Engineering, Myongji University

2. SFR System Design Division, Korea Atomic Energy Research Institute (KAERI)

3. Department of Extreme Energy Systems, Korea Institute of Machinery and Materials (KIMM)

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/61/6/61_T-17-74/_pdf

Reference21 articles.

1. 1) Weinberg, M. and Wyzykowski, J.: Powering Unmanned Air Craft, Aerospace Engineering, 21 (2000), pp. 23–26.

2. 2) U. S. Standard Atmosphere, NASA-TM-X-7433b, 1976.

3. 3) Castner, R., Chiappetta, S., Wyzykowski, J., and Adamczyk, J.: An Engine Research Program Focused on Low Pressure Turbine Aerodynamic Performance, GT-2002-3004, 2002.

4. 4) Fielding, L.: Turbine Design, ASME Press, New York, 2000, pp. 27–28.

5. 5) Van Treuren, K. W., Simon, T., Von Koller, M., Byerley, A. R., Baughn, J. W., and Rivir, R.: Measurements in a Turbine Cascade Flow under Ultra Low Reynolds Number Conditions, J. Turbomach., 124 (2002), pp. 100–106.

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