The invention discloses an aerodynamic
data processing method for an aircraft. The method comprises the following steps: S1, performing classification according to control surfaces, establishing hierarchical relationship names for aerodynamic data of each control surface according to the height, a Mach number, a
yaw angle and a
rudder deviation, and establishing a data object by using an object-oriented thought; S2, reading original aerodynamic data through an original aerodynamic data reading module, establishing a
data structure body, and performing primary analysis on
original data through an aerodynamic primary analysis module; S3, according to
data processing process and method, establishing a process-oriented data computing process; and S4, generating a universal
database through an aerodynamic
data processing system for the aircraft. The invention furthermore provides the aerodynamic
data processing system used for implementing the aerodynamic data
processing method. The method and
system have the beneficial effects that the post-
processing burden is reduced, the error rate is low, the computing process work can be reused in data
processing of different stages, and lots of working time is saved.