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R. Asokan

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Open access Aug 2026

Concurrent Aero-Structural Optimization and Mission Weight and Centre of Gravity Assessment for Weaponized Helicopter Conversion

 This multidisciplinary approach seeks to determine how to upgrade a civilian helicopter to a weapons-capable design by optimizing both integrated aero-structural and mission parameters. The finite element analysis (FEA), computational fluid dynamics (CFD) and key parameters to assess the integrity of components (struc...

D. Kumaresan, R. Asokan, C. J. Babu et al. · 0 citations

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