Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load.
Interim rept. 1 Feb 74-31 Jan 75,
GEORGIA INST OF TECH ATLANTA SCHOOL OF ENGINEERING SCIENCE AND MECHANICS
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This report contains a technical procedure by which one may design a fuselage type stiffened thin curcular cylindrical shell to carry safely a specified destabilizing load uniform axial compression, uniform pressure, and torsion individually applied.
- *Stiffened cylinders
- Shells(Structural forms)
- Dynamic loads
- Load distribution
- Thin walls
- Hydrostatic pressure
- Yield strength
- Ring stiffened cylinders
- Trade off analyses
- Partial differential equations
- Structural Engineering and Building Technology