DSpace - NTUA (National Technical University of Athens) · 2002 · 20 citations · 12 references
Open access
EngineeringAerospace EngineeringComputational EngineeringAcousticsAerodynamicsComputational Fluid DynamicsAeroacousticsAeroacoustics SimulationAeroelastic ModelingComputational AerodynamicsRotorcraft AerodynamicsUnsteady AerodynamicsAerodynamic EfficiencyAerodynamic LoadsAerodynamic ModelingComputational AeroacousticsComputational EfficiencyComputational Efficiency AnalysisRotor Wake DynamicsRotorcraft Aeroacoustics
The initial development of a combined active aeroelastic aeroacoustic rotorcraft code is discussed. The GENeral Unsteady Vortex Particle code (GENUVP) is used as the aerodynamic component of the combined code. A brief discussion of the theory behind GENUVP's use of an unsteady panel method with a vortex particle wake is presented. Modifications to GENUVP to increase its computational efficiency are
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