Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19660044313

Stability of axially compressed core-filled cylinders.

View original source ↗Export metadata ↓

Abstract

Stability and buckling of core-filled axially compressed circular cylinder

Explore related subjects

SHELL STABILITY SHEARING STRESS CIRCULAR CYLINDER ELASTIC BUCKLING AXIAL COMPRESSION

Keep this discovery

Explore connections, maps & timelines

Myint-U, T.. 1966-03-01. Stability of axially compressed core-filled cylinders.. https://ntrs.nasa.gov/citations/19660044313

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Buckling of spherical shells ring-supported at the edges.

Elastic buckling loads of shallow spherical shells supported by edge rings including nonlinear prebuckling effects

SHELL STABILITY↗

NASA NTRS1967

Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0

Configuration modifications of tension shell shapes to improve aerodynamic characteristics at Mach 3 by delaying onset of flow separation

SHELL STABILITY↗

NASA NTRS1967

A theoretical and experimental investigation of shear lag in stiffened shells and the stress analysis of cone frustums and segments Final report

Shear lag effect on stress distribution in stiffened shells, and stress analysis of cone frustums and segments

SHELL STABILITY↗