Journal
AIAA JOURNAL
Volume 57, Issue 10, Pages 4328-4342Publisher
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.J057575
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Funding
- Brazilian National Council for Scientific and Technological Development
- University of Michigan
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An enhanced nonlinear aeroelastic-coupled-flight dynamics framework that enables the investigation of propeller aerodynamics and inertial effects on the response of a very flexible aircraft is presented, verified and used to investigate the propeller effects on the aeroelastic response of a very flexible aircraft. The developed framework couples a geometrically nonlinear structural solver with an unsteady vortex lattice method for lifting surfaces and a viscous vortex particle for propeller slipstream. Propeller gyroscopic moment and viscous drag estimation for unsteady vortex lattice method are also included. For the study case considered, the University of Michigan's X-HALE unmanned aerial vehicle model, results indicate that the influence of propeller is more pronounced for free-flight cases and in clamped cases involving torsional excitation.
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