ASSESSMENT OF AN ADAPTIVE ONE-EQUATION TURBULENCE MODEL FOR LEADING EDGE VORTEX FLOWS ON MULTIPLE SWEPT DELTA WINGS

Keyphrases

• Turbulence Model 100%
• Vortex Flow 100%
• Delta Wing 100%
• Leading Edge Vortex 100%
• One-equation Turbulence Model 100%
• Computational Fluid Dynamics Simulation 66%
• Angle of Attack 66%
• Mach number 33%
• Flow Field 33%
• Design Phase 33%
• Aircraft Design 33%
• Aerospace Applications 33%
• High Agility 33%
• Sideslip Angle 33%
• Control Surface Deflection 33%
• Low Aspect Ratio Wing 33%
• Eddy Viscosity Turbulence Models 33%
• Complex Turbulence 33%
• Spalart-Allmaras Turbulence Model 33%
• Boussinesq Assumption 33%

Engineering

• Leading Edge Vortex 100%
• Vortex Flow 100%
• Delta Wing 100%
• Equation Turbulence Model 100%
• Computational Fluid Dynamics 66%
• Mach Number 33%
• Angle-of-Attack 33%
• Aerospace Applications 33%
• Low Aspect Ratio Wings 33%
• Boussinesq's Hypothesis 33%
• Design Phase 33%
• Control Surfaces 33%
• Eddy Viscosity 33%
• Attack Angle 33%
• Flow Distribution 33%

Physics

• Turbulence Model 100%
• Vortex 100%
• Computational Fluid Dynamics 40%
• Flow Distribution 20%
• Aircraft Design 20%
• Angle of Attack 20%
• Aspect Ratio 20%
• Mach Number 20%
• Eddy Viscosity 20%
• Control Surfaces 20%