Pages that link to "Item:Q3552150"
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The following pages link to Aerodynamic shape optimization on overset grids using the adjoint method (Q3552150):
Displaying 11 items.
- A comparison of the continuous and discrete adjoint approach extended based on the standard lattice Boltzmann method in flow field inverse optimization problems (Q293688) (← links)
- An adaptive grid method for analysis of 3D aircraft configurations (Q686948) (← links)
- Development of an efficient aerodynamic shape optimization framework (Q1025325) (← links)
- A multigrid overset grid flow solver with implicit hole cutting method (Q1033186) (← links)
- Aerodynamic optimal shape design based on body-fitted grid generation (Q1718558) (← links)
- Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers (Q1973769) (← links)
- Adjoint-assisted Pareto front tracing in aerodynamic and conjugate heat transfer shape optimization (Q2028109) (← links)
- A preconditioned multiple shooting shadowing algorithm for the sensitivity analysis of chaotic systems (Q2222553) (← links)
- Multigrid One-Shot Method for State Constrained Aerodynamic Shape Optimization (Q3648617) (← links)
- A surface mesh movement algorithm for aerodynamic optimization of the nacelle position on wing-body-nacelle-pylon configuration (Q5371888) (← links)
- Effect of grid displacement models on sensitivity derivatives computed by the continuous adjoint method in aerodynamic and conjugate heat transfer shape optimization (Q6094375) (← links)
