Innovative numerical techniques for two dimensional elastic and elastic-plastic multiple crack problems are presented using micromechanics concepts and complex variables. The simplicity and the accuracy of the proposed method will enable us to carry out the multiple-site fatigue crack propagation analyses for airplane fuselage by incorporating such features as the curvilinear crack path, plastic deformation, coalescence of cracks, etc.
Study of multiple cracks in airplane fuselage by micromechanics and complex variables
1994-09-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Effect of pressurization on airplane fuselage drag.
AIAA | 1965
|Pressurized airplane fuselage, comprising a pressure bulkhead
Europäisches Patentamt | 2018
|