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Experimental and Numerical Nonlinear Stability Analysis of Wings Incorporating Flared Folding Wingtips (2024)

First Author: Healy F

Attributed to: Purchase of Six Component Wind Tunnel Balance funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/1.c037167

Publication URI: http://dx.doi.org/10.2514/1.c037167

Type: Journal Article/Review

Parent Publication: Journal of Aircraft

Issue: 1