Numerical investigation of engine position effects on contrail formation and evolution in the near-field of a realistic aircraft configuration

Keyphrases

• Numerical Investigation 100%
• Adsorption 100%
• Contrails 100%
• Soot 100%
• Aircraft Configuration 100%
• Water Vapor 100%
• Ice Crystals 100%
• Position Effect 100%
• Contrail Formation 100%
• Near-field 100%
• Engine Position 100%
• Mesh Adaptation 50%
• Three-dimensional (3D) 50%
• Process Structure 50%
• Particle Distribution 50%
• Vortex Interactions 50%
• Plume 50%
• Sulfur Species 50%
• Microphysical Model 50%
• Soot Particles 50%
• Optical Properties 50%
• Number Concentration 50%
• Reynolds-averaged Navier-Stokes 50%
• Optical Thickness 50%
• Fuselage 50%
• Access to Water 50%
• Adaptation Techniques 50%
• Strong Dependence 50%
• Eulerian 50%
• Detailed numerical Simulation 50%
• Microphysical 50%
• Low Activation 50%
• Field Evolution 50%
• Emission Index 50%
• Wake Structure 50%
• Engine Placement 50%
• Boeing 777 50%
• Ice nucleation 50%
• Number Emissions 50%
• Dilution Condition 50%
• Ice Crystal Properties 50%
• Plume Temperature 50%
• Tailplane 50%
• Depletion Effect 50%
• Relative Humidity 50%
• Dilution Method 50%

Engineering

• Dilution 100%
• Aircraft 100%
• Ice Crystal 75%
• Computer Simulation 25%
• Reynolds-Averaged Navier-Stokes 25%
• Relative Humidity 25%
• Jet 25%
• Tailplane 25%