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 		Structural stability under shear stress of an aircraft fuselage shell

Thesis 1: EXTRA 400 | Thesis 2: Fatigue tests | Diploma Thesis: Fuselage structure analysis


Carried out at

Institut für Leichtbau der RWTH Aachen
Dept. of Aerospace Structures, Aachen University of Technology


Subjects/Tasks:

  • Computer-aided design with pre-processing software MSC PATRAN of a fuselage structure
  • Finite-element analysis of a frame/stringer reinforced fuselage structure with MSC NASTRAN processor
  • Programming of post-processing FORTRAN routines
  • Post-processing with post-processing software MSC PATRAN / NASTRAN
  • Modification and improvement of existing formulas to analyse known problems with frame/stringer reinforced fuselage structures
  • Analysis of results & interpretation


More information coming soon!




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Torsten Anft:
About Torsten Anft | Thesis 1: EXTRA 400 | Thesis 2: Fatigue tests
Diploma Thesis: Fuselage structure analysis

F-14 Tomcat:
History | Specifications | Bureau Numbers | Walk-Around | Squadrons | Photos | Books | Memorabilia

Other Topics:
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