Correction: Nonlinear Aeroelastic Model Considering RANS Unsteady Aerodynamics with Dynamically Linearized Time-domain Approach (American Institute of Aeronautics and Astronautics Inc, AIAA)

Correction Notice Subsection III.B.2. Table 1: the boundary layer thickness percentage from the ReD configuration at x/a = 0 is as indicated in red below. (Table presented).

Duke Scholars

Author Earl H. Dowell Thomas Lord Department of Mechanical Engineering and Materia ...