NASA Technical Reports Server (NTRS) 19850014037: Study for prediction of rotor-wake-fuselage interference. Part 2: Program users guideReport as inadecuate




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A method was developed which permits the fully coupled calculation of fuselage and rotor airloads for typical helicopter configurations in forward flight. To do this, an iterative solution is carried out based on a conventional panel representation of the fuselage and a blade element representation of the rotor where fuselage and rotor singularity

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/



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