Nonlinear reduced-order modeling of the forced and autonomous aeroelastic response of a membrane wing using Harmonic Balance methods.

MLA

Nardini, Massimiliano, et al. “Nonlinear Reduced-Order Modeling of the Forced and Autonomous Aeroelastic Response of a Membrane Wing Using Harmonic Balance Methods.” Journal of Fluids & Structures, vol. 91, Nov. 2019, p. N.PAG. EBSCOhost, https://doi.org/10.1016/j.jfluidstructs.2019.102699.

APA

Nardini, M., Illingworth, S. J., & Sandberg, R. D. (2019). Nonlinear reduced-order modeling of the forced and autonomous aeroelastic response of a membrane wing using Harmonic Balance methods. Journal of Fluids & Structures, 91, N.PAG. https://doi.org/10.1016/j.jfluidstructs.2019.102699

Chicago

Nardini, Massimiliano, Simon J. Illingworth, and Richard D. Sandberg. 2019. “Nonlinear Reduced-Order Modeling of the Forced and Autonomous Aeroelastic Response of a Membrane Wing Using Harmonic Balance Methods.” Journal of Fluids & Structures 91 (November): N.PAG. doi:10.1016/j.jfluidstructs.2019.102699.