Conceptual-level evaluation of a variable stiffness skin for a morphing wing leading edge
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H Haddad Khodaparast | C Wang | MI Friswell | A Magrini | R Ponza | E Benini | V Landersheim | D Laveuve | C Contell Asins
[1] Sergio Ricci,et al. Compliant structures-based wing and wingtip morphing devices , 2016 .
[2] A. Puck,et al. Guidelines for the determination of the parameters in Puck's action plane strength criterion , 2002 .
[3] Johannes Riemenschneider,et al. DLR's Morphing Wing Activities within the European Network , 2014 .
[4] Sergio Ricci,et al. A Two-Level Approach for the Optimal Design of Morphing Wings Based On Compliant Structures , 2011 .
[5] Peter Horst,et al. Three-dimensional design of a large-displacement morphing wing droop nose device , 2018 .
[6] Ernesto Benini,et al. Comparison of Constrained Parameterisation Strategies for Aerodynamic Optimisation of Morphing Leading Edge Airfoil , 2019 .
[7] Z. Gürdal,et al. Variable-stiffness composite panels: Buckling and first-ply failure improvements over straight-fibre laminates , 2008 .
[8] Zafer Gürdal,et al. Optimization of a composite cylinder under bending by tailoring stiffness properties in circumferential direction , 2010 .
[9] Mostafa Abdalla,et al. Optimization of a variable-stiffness skin for morphing high-lift devices , 2010 .
[10] Ruxandra Botez,et al. Aerodynamic performance improvement of the UAS-S4 Éhecatl morphing airfoil using novel optimization techniques , 2016 .
[11] Ernesto Benini,et al. Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization , 2018 .
[12] H. Schürmann,et al. FAILURE ANALYSIS OF FRP LAMINATES BY MEANS OF PHYSICALLY BASED PHENOMENOLOGICAL MODELS , 1998 .
[13] Peter Horst,et al. Extremely deformable morphing leading edge: Optimization, design and structural testing , 2017 .
[14] Hans Peter Monner,et al. DESIGN OF A SMART LEADING EDGE DEVICE FOR LOW SPEED WIND TUNNEL TESTS IN THE EUROPEAN PROJECT SADE , 2011 .
[15] Jonathan E. Cooper,et al. Aeroelastic Tailoring of a Representative Wing-Box Using Tow-Steered Composites , 2017 .
[16] Johannes Riemenschneider,et al. Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests , 2017 .
[17] Fabrizio Scarpa,et al. Evaluation of hexagonal chiral structure for morphing airfoil concept , 2005 .