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- W28008354 abstract "An analytical method has been developed to treat unsteady helicopter rotor, wake, and fuselage interaction aerodynamics. An existing lifting line/prescribed wake rotor analysis and a source panel fuselage analysis were modified to predict vibratory fuselage airloads. The analyses were coupled through the induced flow velocities of the rotor and wake on the fuselage and the fuselage on the rotor. A prescribed displacement technique was used to distort the rotor wake about the fuselage. Sensitivity studies were performed to determine the influence of wake and body geometry on the computed airloads. Predicted and measured mean and unsteady pressures on a cylindrical body in the wake of a two-bladed rotor were compared. Initial results show good qualitative agreement." @default.
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- W28008354 date "1987-01-01" @default.
- W28008354 modified "2023-09-27" @default.
- W28008354 title "An unsteady rotor/fuselage interaction method" @default.
- W28008354 hasPublicationYear "1987" @default.
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