NASA NTRS · 20200005202
TPSAS-NF1676L-31914-DND
Abstract
Analysis of aircraft systems involves many disciplines: aerodynamics, structural dynamics, aeroacoustics, etc. - rotorcraft aeromechanics is a typical example. Gradient-based, multidisciplinary optimization (MDO) requires sensitivity analysis for all disciplines. Adjoint-based sensitivity analysis capabilities for: - Coupled aero/structure FUN3D/DYMORE system; - Coupled aero/acoustics FUN3D/ANOPP2 system.
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Li Wang. TPSAS-NF1676L-31914-DND. https://ntrs.nasa.gov/citations/20200005202
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