power_monger
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During the year 2013-14, the R&D divisions at NAL have significantly contributed towards the Advanced Medium Combat Aircraft programme of Aeronautical Development
Agency (ADA). The R&D efforts led to the new configuration AMCA-3B-08 and a structurally efficient wing layout with four bending attachment brackets and two shear attachment brackets. For the AMCA 3B-08, structural design, analysis and size optimization was carried out to cater for all critical symmetric and un-symmetric load cases. Finite element models were built separately for each of the fuselage segments and then integrated to build a full fuselage finite element model.
AMCA Version 3B-08
Agency (ADA). The R&D efforts led to the new configuration AMCA-3B-08 and a structurally efficient wing layout with four bending attachment brackets and two shear attachment brackets. For the AMCA 3B-08, structural design, analysis and size optimization was carried out to cater for all critical symmetric and un-symmetric load cases. Finite element models were built separately for each of the fuselage segments and then integrated to build a full fuselage finite element model.
AMCA Version 3B-08
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