Clark-Y airfoil performance at low Reynolds numbers-Reference-Cited by-同舟云学术

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Clark-Y airfoil performance at low Reynolds numbers

Published:1984-01-09 Issue: Volume: Page:
ISSN:
Container-title:22nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

MARCHMAN, III J.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-52

Reference8 articles.

1. Distribution Investigation i n the Variable Density Wind Tunnel," NACA Report No. 353, 1930.

2. Clark-Y airfoil i s an able performer a t Reynolds numbers above approximately 75,000. I n the Re range from 75,000-200,000 it i s possible to obtain

3. CL vs FOR PI-60 AIRFOIL AT RE = 168000(1)

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