Smoother Wing Leading-Edge Joints Would Favor Laminar Flow

TBMG-29923

06/01/1999

Abstract
Content

Some changes in the design and construction of the leading edges of metal airplane wings have shown promise as means to suppress laminar-to-turbulent flow transitions. The significance of this development is that it creates an opportunity to take advantage of laminar-flow boundary layers to reduce aerodynamic drag.

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Citation
"Smoother Wing Leading-Edge Joints Would Favor Laminar Flow," Mobility Engineering, June 1, 1999.
Additional Details
Publisher
Published
Jun 1, 1999
Product Code
TBMG-29923
Content Type
Magazine Article
Language
English