Buckling Alleviation for Joined-Wing Aircraft
نویسندگان
چکیده
منابع مشابه
Nonlinear Aeroelastic Analysis of Joined-wing Aircraft
Joined-wing aircraft are being designed for ‘sensorcraft’ configuration. Joined wings lead to multiple load paths and constraints. The focus of this work is to understand the nonlinear structural as well as aeroelastic behavior of joined wings. The paper presents a formulation for the nonlinear aeroelastic analysis of joined wings. Results are presented for two joined wings configurations. Over...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2016
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.c033426