Effects of Low Reynolds Numbers on Performance of a One-Stage Axial Compressor-Reference-Cited by-同舟云学术

Effects of Low Reynolds Numbers on Performance of a One-Stage Axial Compressor

Published:2015 Issue:5 Volume:58 Page:280-288
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 Tae-Gon¹,JUNG Young-Jin¹,JUNG Yohan²,CHOI Minsuk¹

Affiliation:

1. Department of Mechanical Engineering, Myongji University

2. Fluid Machinery Research Department, Hyundai Heavy Industries Co., Ltd.

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/58/5/58_T-14-73/_pdf

Reference14 articles.

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

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

4. 4) Schreiber, H.-A., Steinert, W., and Küsters, B.: Effects of Reynolds Number and Free-stream Turbulence on Boundary Layer Transition in a Compressor Cascade, J. Turbomach., 124 (2002), pp. 1–9.

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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