NASA Technical Reports Server (NTRS) 19840005089: Analytical model of rotor wake aerodynamics in ground effectReport as inadecuate




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The model and the computer program developed provides the velocity, location, and circulation of the tip vortices of a two-blade helicopter in and out of the ground effect. Comparison of the theoretical results with some experimental measurements for the location of the wake indicate that there is excellent accuracy in the vicinity of the rotor and

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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