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Investigation Of Rotor Response To Vibratory Aerodynamic Inputs. Part 3. Threedimensional Effects On Unsteady Flow Through A Helicopter Rotor
Author(s): Ashley, Holt, Moser, Herbert H., Dugundji, JohnCorporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-10
Report number: WADC TR 58-87 Part 3
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