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Aircraft Modeling and Simulation
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Various aerodynamics, structural dynamics, and control design and experimental studies are presented with the aim of advancing green and morphing aircraft research. The results obtained with an in-house CFD code are compared and validated with those of two NASA codes. The aerodynamical model of the UAS-S45 morphing wing as well as the structural model of a morphing winglet are presented. A new design methodology for oleo-pneumatic landing gear drop impact dynamics is presented as well as its experimental validation. The design of a nonlinear dynamic inversion (NDI)-based disturbance rejection control on a tailless aircraft is presented, including its validation using wind tunnel tests.
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Keywords
- adaptive structures
- aerodynamic performance
- airfoil flow
- anti-windup
- backward-facing step flow
- cascade flow
- computational fluid dynamics
- disturbance observer
- drop impact
- FE modeling
- flat plate flow
- flight tests
- ground loads
- History of engineering & technology
- landing gear dynamics
- loads assessment
- morphing airfoil optimization
- n/a
- nonlinear dynamic inversion
- oleo-pneumatic shock absorber
- parameterization
- PSO
- spin-up
- spring-back
- stress analysis
- tailless aircraft
- Technology, engineering, agriculture
- Technology: general issues
- turbulence modeling
- wind tunnel
Links
DOI: 10.3390/books978-3-0365-3211-0Editions