Comparative studies of numerical methods for evaluating aerodynamic characteristics of two-dimensional airfoil at low Reynolds numbers-Reference-Cited by-同舟云学术

Comparative studies of numerical methods for evaluating aerodynamic characteristics of two-dimensional airfoil at low Reynolds numbers

Published:2017-01-02 Issue:1 Volume:31 Page:57-67
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Lee D.¹,Nonomura T.²,Oyama A.²,Fujii K.³

Affiliation:

1. Department of Aeronautics and Astronautics, University of Tokyo, Sagamihara, Japan

2. Department of Space Transportation Engineering, Institute of Space and Astronautical Science/JAXA, Sagamihara, Japan

3. Department of Information Science, Tokyo University of Science, Tokyo, Japan

Funder

JSPS

Scientific Research (A)

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2016.1274398

Reference44 articles.

1. Low-Reynolds Number Aerodynamics of Airfoils at Incidence

2. Intermittent Bursting of a Laminar Separation Bubble on an Airfoil

3. Computational and Experimental Analysis of a High-Performance Airfoil Under Low-Reynolds-Number Flow Condition

4. Thin-layer approximation and algebraic model for separated turbulentflows

5. Carmichael, B.H. 1982. “Low Reynolds Number Airfoil Survey.” NASA-CR-165803.

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