NASA NTRS · 19800006791
A parametric wing design study for a modern laminar flow wing
Abstract
The results of a parametric wing design study using a modern laminar flow airfoil designed to exhibit desirable stall characteristics while maintaining high cruise performance are presented. It was found that little is sacrificed in cruise performance when satisfying the stall margin requirements if a taper ratio of 0.65 or greater is used.
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Koegler, J. A., Jr.. 1979-12-01. A parametric wing design study for a modern laminar flow wing. https://ntrs.nasa.gov/citations/19800006791
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