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Research is concerned with determining the sensitivity of various aerolastic responses such as divergence, flutter, aerolastic lift distribution, and control effectiveness to small perturbations in the shape parameters of the wing. The wing parameters of interest are sweep, aspect ratio, taper ratio, wing surface area, and the root angle of attack. Emphasis is on determining these sensitivities using analytical methods as opposed to the finite difference method. Research also involves developing CFD/CSD interaction methodology.
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Aerospace Science and Technologypp.109171, (2024)
Apurba Sarkar,Aniket Jana, Atharva Agashe,Ji Wang,Rakesh Kapania,Nir S Gov,Jennifer G DeLuca,Raja Paul, Amrinder S Nain
bioRxiv : the preprint server for biology (2024)
Structural and Multidisciplinary Optimizationno. 1 (2023): 1-20
AIAA SCITECH 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
AIAA JOURNALno. 3 (2023): 1349-1365
AIAA JOURNALno. 10 (2023): 4632-4651
Sudharsan Parthasarathy,Rakesh K. Kapania
AIAA SCITECH 2023 Forum (2023)
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