Accession Number:

ADA017657

Title:

Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load.

Descriptive Note:

Interim rept. 1 Feb 74-31 Jan 75,

Corporate Author:

GEORGIA INST OF TECH ATLANTA SCHOOL OF ENGINEERING SCIENCE AND MECHANICS

Report Date:

1975-02-01

Pagination or Media Count:

104.0

Abstract:

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.

Subject Categories:

  • Aircraft
  • Structural Engineering and Building Technology
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE