Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Numerical Simulations of the HVAB Rotor in Hover
A PHYSICS-BASED MODEL FOR INFLOW CHARACTERISTICS OF MULTI-ROTOR CONFIGURATIONS
A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers
A new rotorcraft design framework based on reliability and cost
Development of a Sonic Sensor for Aircraft Applications
A Unified Approach for Modeling Fluid-Structure Interactions of Large-Scale Offshore Wind Turbines
Aerodynamics and aeroacoustic sources of a coaxial rotor
Application of Extended Messinger Model for Ice Accretion on Complex Geometries
Computational fluid dynamics simulation of three-dimensional parallel jets
Assessment of the icing characteristics of single and coaxial rotors