Investigation Of Rotor Response To Vibratory Aerodynamic Inputs. Part 3. Threedimensional Effects On Unsteady Flow Through A Helicopter Rotor

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Report Number: WADC TR 58-87 Part 3
Author(s): Ashley, Holt, Moser, Herbert H., Dugundji, John
Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Date of Publication: 1958-10
Pages: 88
DoD Task:
PB Number: PB156304-3

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