Aeroelastic Analysis of a Joined-Wing Sensorcraft
Jennifer J. Sitz
Broschiertes Buch

Aeroelastic Analysis of a Joined-Wing Sensorcraft

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This study performed an aeroelastic analysis of a joined-wing SensorCraft. The analysis was completed using an aluminum structural model that was splined to an aerodynamic panel model. The force and pressure distributions were examined for the four aerodynamic panels: aft wing, fore wing, joint, and outboard tip. Both distributions provide the expected results (elliptical distribution), with the exception of the fore wing. The fore wing appears to be affected by interference with the joint. The use of control surfaces for lift and roll was analyzed. Control surfaces were effective throughout m...