Pages that link to "Item:Q2171508"
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The following pages link to Finite element methodology for modeling aircraft aerodynamics: development, simulation, and validation (Q2171508):
Displaying 13 items.
- Isogeometric blended shells for dynamic analysis: simulating aircraft takeoff and the resulting fatigue damage on the horizontal stabilizer (Q2086059) (← links)
- Application of finite element method in aeroelasticity (Q2483322) (← links)
- Direct immersogeometric fluid flow and heat transfer analysis of objects represented by point clouds (Q2678475) (← links)
- An efficient aerodynamic boundary element method for aeroelastic simulations and its experimental validation (Q3044565) (← links)
- Application of the finite element technique to aerodynamic problems of aircraft (Q3342051) (← links)
- (Q3421174) (← links)
- Finite element analysis of lift build‐up due to aerofoil indicial motion (Q4273126) (← links)
- Accurate finite element method for steady and quasisteady lifting aerofoil (Q4286462) (← links)
- Application of the finite element method to aeroelasticity (Q4943089) (← links)
- Fluid–structure interaction modeling with nonmatching interface discretizations for compressible flow problems: Computational framework and validation study (Q6099249) (← links)
- Isogeometric analysis in computation of complex-geometry flow problems with moving boundaries and interfaces (Q6125051) (← links)
- Fluid-structure interaction modeling with nonmatching interface discretizations for compressible flow problems: simulating aircraft tail buffeting (Q6604130) (← links)
- \textit{Quo vadis}, wave? Dispersive-SUPG for direct van der Waals simulation (DVS) (Q6663272) (← links)
