Objectives: Reliable evaluation of mass flow rates through permeable boundaries - Estimate and control discretization error- Consider both computational domain outflow and inflow- Applicable to simulating propulsion-system effects, as well as secondary flow paths - Explore feasibility of handling more general outputs at domain boundaries. Design optimization subject to mass-flow-rate constraints - Improve aerodynamic performance and reduce noise due to sonic boom - Control discretization error in design space to improve confidence in final designs.
Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion
AIAA Aviation and Aeronautics Forum (Aviation 2019) ; 2019 ; Dallas, TX, United States
20.06.2019
Sonstige
Keine Angabe
Englisch
AIAA-2019-3488: Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion
British Library Conference Proceedings | 2019
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