Inclusion of transverse shear deformation in optimum design of aircraft wing panels

Phil W. L. Williams,Fred W. Williams

Inclusion of transverse shear deformation in optimum design of aircraft wing panels

1996

Phil W. L. Williams
Fred W. Williams

The effects of shear deformation plate theory on the minimum mass design of composite prismatic plate assemblies of practical aircraft wing panel proportions are investigated using VICONOPT

Keywords:

Plate theory
Buckling
Structural engineering
Transverse plane
Wing
Deformation (mechanics)
Mathematics
Composite number
Minimum mass
transverse shear deformation
Numerical analysis

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