NASA NTRS · 19760003914
Drag Reduction: Back to Basics
Abstract
Aeronautical design engineering for general aviation aircraft considers the iteration of wind tunnel test data are lift, weight, drag, and thrust as the basic balancing factor in drag reduction efforts.
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Nicks, O. W.. 1975-01-01. Drag Reduction: Back to Basics. https://ntrs.nasa.gov/citations/19760003914
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