'A NEW CFD APPROACH FOR THE COMPUTATION OF GENERAL ROTORCRAFT FLOWS' THE COMPUTATION OF ROTARY WING AERODYNAMICS BY COMPUTATIONAL FLUID DYNAMICS IS VERY DIFFICULT BECAUSE OF THE DOMINANCE OF THE VORTICAL WAKE. NOT ONLY IS THE WAKE REGION VERY LARGE AND IN

Project: Research project

Project Details

Description

'A New CFD Approach for the Computation of General Rotorcraft Flows' The computation of rotary wing aerodynamics by Computational Fluid dynamics is very difficult because of the dominance of the vortical wake. Not only is the wake region very large and in

StatusFinished
Effective start/end date9/1/081/26/11

Funding

  • National Aeronautics and Space Administration: $193,294.00

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