Negative lift characteristics of NACA 0012 aerofoil at low Reynolds numbers-Reference-Cited by-同舟云学术

Negative lift characteristics of NACA 0012 aerofoil at low Reynolds numbers

Published:2019-01 Issue:1 Volume:44 Page:
ISSN:0256-2499
Container-title:Sādhanā
language:en
Short-container-title:Sādhanā

Author:

Pranesh C,Sivapragasam M^ORCID,Deshpande M D,Narahari H K

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Link

http://link.springer.com/article/10.1007/s12046-018-1008-6/fulltext.html

Reference10 articles.

1. Mueller T J and Batill S M 1982 Experimental studies of separation on a two-dimensional airfoil at low Reynolds numbers. AIAA J. 20: 457–463

2. Ohtake T, Nakae Y and Motohashi T 2007 Nonlinearity of the aerodynamic characteristics of NACA0012 aerofoil at low Reynolds numbers. J. Jpn. Soc. Aeronaut. Space Sci. 55: 439–445

3. Tank J, Smith L and Spedding G R 2017 On the possibility (or lack thereof) of agreement between experiment and computation of flows over wings at moderate Reynolds number. Interface Focus 7: 1–15

4. Yonemoto K, Takato K, Ochi H and Fujie S 2008 Kutta condition violation in two-dimensional NACA0012 airfoil at low Reynolds number. AIAA Paper 2008-6399

5. Lee D, Nonomura T, Oyama A and Fujii K 2014 Comparison of numerical methods evaluating airfoil aerodynamic characteristics at low Reynolds number. J. Aircr. 52: 296–306

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