Stiffened panel stability behaviour and performance gains with plate prismatic sub-stiffening
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Adrian Murphy | Damian Quinn | W. McEwan | F. Lemaitre | A. Murphy | D. Quinn | W. McEwan | F. Lemaître
[1] Lei Jiang,et al. A finite element simulation of the test procedure of stiffened panels , 1998 .
[2] S. Metschan,et al. Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs: Cost Assessment of Manufacturing/Design Concepts , 2000 .
[3] Mark Price,et al. Toward Virtual Testing of Airframe Stiffened Panels , 2006 .
[4] Mustafa Özakça,et al. Tailoring Static Strength Performance of Metallic Stiffened Panels by Selective Local Sub-Stiffening , 2006 .
[5] Giuliano Allegri,et al. Design and Modeling of Selective Reinforcements for Integral Aircraft Structures , 2007 .
[6] M. M. Domb,et al. MODELLING OF STIFFENER CRIPPLING PHENOMENA USING FINITE ELEMENT ANALYSIS , 1998 .
[7] J Munroe,et al. Integral Airframe Structures (IAS)---Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs , 2000 .
[8] Gary L. Farley,et al. SELECTIVE REINFORCEMENT TO IMPROVE FRACTURE TOUGHNESS AND FATIGUE CRACK GROWTH RESISTANCE IN METALLIC STRUCTURES , 2004 .
[9] Mark Price,et al. The Computational Post Buckling Analysis Of Fuselage Stiffened Panels Loaded In Compression , 2004 .
[10] Johann Arbocz,et al. Buckling experiments : experimental methods in buckling of thin-walled structures , 2000 .
[11] E. F. Bruhn,et al. Analysis and Design of Flight Vehicle Structures , 1973 .
[12] Richard G. Pettit,et al. Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs , 2000 .