The invention discloses a wing angle adjusting
system and a flight demonstration method, and relates to the technical field of wing
simulation adjustment, the adjusting
system comprises a
wind field simulation module and an
attack angle adjusting module; the
wind field simulation module takes a discrete simulation space as a unit, establishes a
mass conservation equation and a
momentum conservation equation based on a Navier-Stokes equation, and discretizes the
momentum conservation equation into an
algebraic equation set by adopting a second-order windward format and a central difference format; a simulated
wind field is generated through a semi-implicit method of a pressure
coupling equation set according to constraint iteration of an
algebraic equation set and a
mass conservation equation; the
attack angle adjusting module is used for placing the wing 3D model in a simulation space, establishing a model of lift force, resistance and rotation amount about an
attack angle, and iteratively acquiring an optimal attack angle by adopting a
whale optimization
algorithm; according to the demonstration method, demonstration is carried out based on wind
field simulation parameters and the optimal attack angle, an actual wind field
vector diagram and a
wind flow curve are calculated, and accurate simulation of a wind field, attack angle self-adaptive adjustment and matched adjustment demonstration are achieved.