More information: https://www.airshaper.com
Sample project: https://app.airshaper.com/simulations/naca0015-more-lift-full-morph
In this video, we apply aerodynamic shape optimization using the adjoint technique to a 3D NACA 0015 airfoil.
The method runs through a number of cycles, each containing:
- a primal run (normal CFD simulation of the aerodynamics)
- a dual run (adjoint simulation to link the lift improvement goal to the flow field)
- a sensitivity map calculation (to calculate how the surface should be morphed to increase lift)
- a morphing step to implement these suggestions. The morphing is applied to the volume & surface mesh directly
For more information, just get in touch at info@airshaper.com!
Unlock High-Performance Designs with Our Cloud-Based Aerodynamic Simulation Tool
