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Fluid mechanics / Lifting-line theory / Airfoil / Lift coefficient / Lift / Planing / Angle of attack / Potential flow / Foil / Aerodynamics / Aerospace engineering / Fluid dynamics


Document Date: 2006-10-09 20:16:40

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File Size: 1,07 MB

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Company

Lehman / Langley Laboratory / Saunders-Roe Ltd. / /

Facility

Langley Laboratory / /

IndustryTerm

theoretical and experimental solution / analytical solution / /

Organization

NM NMIIONKL AIYIT.SORY COMMITTEE FOR AERONAUTICS Iuflnllllfluluulln / NATIONAL ADVISORY COMMITTEE / /

Person

Ti / Charles L. Shuford / Jr. / /

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