This paper describes a recent development of an integrated fully coupled aeroservoelastic flight dynamic model of the NASA Generic Transport Model (GTM). The integrated model couples nonlinear flight dynamics to a nonlinear aeroelastic model of the GTM. The nonlinearity includes the coupling of the rigid-body aircraft states in the partial derivatives of the aeroelastic angle of attack. Aeroservoelastic modeling of the control surfaces which are modeled by the Variable Camber Continuous Trailing Edge Flap is also conducted. The R.T. Jones' method is implemented to approximate unsteady aerodynamics. Simulations of the GTM are conducted with simulated continuous and discrete gust loads..
Development of an Integrated Nonlinear Aeroservoelastic Flight Dynamic Model of the NASA Generic Transport Model
AIAA SciTech Forum ; 2018 ; Kissimmee, FL, United States
2018-01-08
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2018
|Aeroservoelastic Modeling of a Generic Transport Model
AIAA | 2010
|Aeroservoelastic Modeling of a Generic Transport Model
British Library Conference Proceedings | 2010
|