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Daniel Guggenheim School of Aerospace Engineering
Daniel Guggenheim School of Aerospace Engineering
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A method of computing the pressure distribution on a single-bladed hovering helicopter rotor
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An examination of the effect of the variable part of blade circulation on the induced power requirements of a two-bladed rotor in forward flight by an electromagnetic analog
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A preliminary design to include a stability and control study in hovering flight of a laterally disposed, single-bladed, counter-rotating, two-rotor helicopter with shrouded tail propeller
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