Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion
Author:
Affiliation:
1. NASA Ames Research Center
2. Science and Technology Corporation
Publisher
American Institute of Aeronautics and Astronautics
Reference40 articles.
1. A Method for Reducing Sonic Boom Strength by Tailoring the Shape of the Propulsive Streamtube
2. Wedge Shock and Nozzle Exhaust Plume Interaction in a Supersonic Jet Flow
3. Integrated Nacelle-Wing Shape Optimization for an Ultra-High Bypass Fanjet Installation on a Single-Aisle Transport Configuration
4. An Adjoint-based Aerodynamic Shape Optimization Strategy for Trimmed Aircraft with Active Engines
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1. A Posterior h/p Adaptive Refinement Algorithm for 3-D Goal-Oriented Electromagnetic Problems;IEEE Transactions on Microwave Theory and Techniques;2023-10
2. Goal-Oriented Discretization Error Control in Coupled Nearfield-Farfield Low-Boom Simulations;AIAA AVIATION 2022 Forum;2022-06-20
3. Cartesian Mesh Simulations for the Third AIAA Sonic Boom Prediction Workshop;Journal of Aircraft;2021-08-31
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