Elastic-Plastic Buckling of Aluminum Cylindrical Shells Subjected to Axisymmetric Impulse LoadsSource: Journal of Applied Mechanics:;1974:;volume( 041 ):;issue: 004::page 985Author:D. L. Wesenberg
DOI: 10.1115/1.3423495Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The elastic-plastic buckling of 6061-T4 aluminum, circular cylindrical shells is examined experimentally and analytically. Groups of shells with radius-to-thickness ratios of 100, 200, and 300 were loaded with short-duration axisymmetric pressure pulses. A fast-discharge capacitor bank and current pulse shaping technique are utilized to provide a sine-squared pressure pulse with duration of about 5 μsec, a duration sufficiently short that loading can be considered impulsive. Average peak-to-peak permanent buckling deformations and wave numbers are compared with predictions from a Lagrangian, finite-difference computer code, and good agreement is obtained between measurements and predictions.
keyword(s): Aluminum , Stress , Impulse (Physics) , Pipes , Buckling , Pressure , Deformation , Measurement , Computers , Waves , Circular cylindrical shells , Pulse shaping , Shells AND Thickness ,
|
Collections
Show full item record
contributor author | D. L. Wesenberg | |
date accessioned | 2017-05-09T01:37:20Z | |
date available | 2017-05-09T01:37:20Z | |
date copyright | December, 1974 | |
date issued | 1974 | |
identifier issn | 0021-8936 | |
identifier other | JAMCAV-26023#985_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/164313 | |
description abstract | The elastic-plastic buckling of 6061-T4 aluminum, circular cylindrical shells is examined experimentally and analytically. Groups of shells with radius-to-thickness ratios of 100, 200, and 300 were loaded with short-duration axisymmetric pressure pulses. A fast-discharge capacitor bank and current pulse shaping technique are utilized to provide a sine-squared pressure pulse with duration of about 5 μsec, a duration sufficiently short that loading can be considered impulsive. Average peak-to-peak permanent buckling deformations and wave numbers are compared with predictions from a Lagrangian, finite-difference computer code, and good agreement is obtained between measurements and predictions. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Elastic-Plastic Buckling of Aluminum Cylindrical Shells Subjected to Axisymmetric Impulse Loads | |
type | Journal Paper | |
journal volume | 41 | |
journal issue | 4 | |
journal title | Journal of Applied Mechanics | |
identifier doi | 10.1115/1.3423495 | |
journal fristpage | 985 | |
journal lastpage | 988 | |
identifier eissn | 1528-9036 | |
keywords | Aluminum | |
keywords | Stress | |
keywords | Impulse (Physics) | |
keywords | Pipes | |
keywords | Buckling | |
keywords | Pressure | |
keywords | Deformation | |
keywords | Measurement | |
keywords | Computers | |
keywords | Waves | |
keywords | Circular cylindrical shells | |
keywords | Pulse shaping | |
keywords | Shells AND Thickness | |
tree | Journal of Applied Mechanics:;1974:;volume( 041 ):;issue: 004 | |
contenttype | Fulltext |