Reynolds Number and Freestream Shear Effects on a NACA 0012 Airfoil in the Reynolds Number Range 10,000-30,000-Reference-Cited by-同舟云学术

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Reynolds Number and Freestream Shear Effects on a NACA 0012 Airfoil in the Reynolds Number Range 10,000-30,000

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Albrecht Mitchell B.¹,Olson David A.¹,Naguib Ahmed M.¹,Koochesfahani Manoochehr¹

Affiliation:

1. Michigan State University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1055

Reference24 articles.

1. Symmetrical Joukowsky airfoils in shear flow

2. TWO-DIMENSIONAL AIRFOILS IN SHEAR FLOW. I

3. Aerofoil section characteristics in shear flows

4. Lift on a steady 2-D symmetric airfoil in viscous uniform shear flow

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