The invention discloses a
composite material structural design
verification method for airworthiness certification. The
composite material structural design
verification method for airworthiness certification comprises the following steps that 1, the application positions of composite materials are determined, and airworthiness
verification of the composite materials is performed; 2, the preliminary dimension of the typic structure is determined, the needed
composite material is selected from the composite
material system determined in the first step, and airworthiness verification is performed on design allowable values of the composite material in the structural state; 3, according to the design allowable values obtained in the second step,
assembly-level detailed design and airworthiness verification of the composite
material structure are performed; 4, according to the structural design of the
assembly-level composite material in the third step, the detailed design and trial trip verification of the composite material of full-scale-level of an
airplane are determined. The composite material structural design verification method has the advantages that the confidence coefficient of a result obtained through the experimental verification method is high, the requirement for experience of designers is low, different persons can follow the same verification method, the certification time is shortened, and the product
development period is shortened.