Some Effects of Camber on Swept-Back Wings

730298

02/01/1973

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
The effects of camber of airfoil sections and wings on the pitching moment coefficient (CM) and on life coefficient (CLo) are examined. Except for changes in CM caused by the wing planform, not-so-slender wings behave similarly to the airfoil sections. The effects of wing planform geometry, however, often overpower the section characteristics. This is particularly true of slender wings with their highly cambered sections which may have multiple sets of coronet vortices.
Wind tunnel tests are compared with the tests of Nangia and Hancock to investigate the mechanism of vortex lift on a cambered wing.
Meta TagsDetails
DOI
https://doi.org/10.4271/730298
Pages
12
Citation
Snyder, M., "Some Effects of Camber on Swept-Back Wings," SAE Technical Paper 730298, 1973, https://doi.org/10.4271/730298.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730298
Content Type
Technical Paper
Language
English