Powerflow simulations of helicopters in blade-vortex interaction conditions

INIS

• helicopters 100%
• simulation 100%
• interactions 100%
• vortices 100%
• rotors 100%
• control 66%
• surfaces 66%
• solutions 66%
• prediction 33%
• air 33%
• benchmarks 33%
• elasticity 33%
• harmonics 33%
• boltzmann equation 33%
• deformation 33%
• motion 33%
• geometry 33%
• noise 33%
• body fluids 33%
• jets 33%
• wind tunnels 33%
• aerodynamics 33%
• acoustics 33%
• boundary conditions 33%
• accuracy 33%
• velocity 33%
• torsion 33%
• walls 33%
• configuration 33%
• large-eddy simulation 33%
• inclusions 33%

Engineering

• Blade Vortex Interaction 100%
• Helicopters 100%
• Boltzmann Equation 100%
• Velocity 50%
• Test Section 50%
• Body Force 50%
• Models 50%
• Fluid 50%
• Simulation Method 50%
• Blade Surface 50%
• Elastic Deformation 50%
• Large Eddy Simulation 50%
• Applied Field 50%
• Benchmark 50%
• Computational Fluid Dynamics 50%
• Transients 50%
• Deflection 50%
• Assuming 50%
• Helicopter Rotors 50%
• Rotor Blade 50%
• Flow Solution 50%
• Harmonics 50%
• Main Rotor 50%
• Aerodynamics 50%
• Tunnels 50%
• Acoustic Far Field 50%