THERMO-MECHANICAL EFFECTS OF INTENSE THERMAL HEATING ON MATERIALS/STRUCTURES.

C. I. Chang; C. A. Griffis; F. R. Stonesifer; J. A. Nemes

doi:10.2514/6.1986-464

THERMO-MECHANICAL EFFECTS OF INTENSE THERMAL HEATING ON MATERIALS/STRUCTURES.

C. I. Chang, C. A. Griffis, F. R. Stonesifer, J. A. Nemes

Research output: Contribution to journal › Conference article › peer-review

3 Scopus citations

Abstract

An analytical methodology for prediction of the response of metallic and composite structures subjected to combined intense heating and applied mechanical loading is presented. The proposed methodology includes a thermal analysis which incorporates nonlinear phenomena such as temperature-dependent thermophysical properties, reirradiation losses, and ablation/melting phenomena. A detailed description of a sequential, finite element, ply-by-ply failure analysis based on the maximum stress criterion is given for composite structures as well as a limit analysis approach for metallic structures. Computational projections are substantiated by experimental measurements for an aerospace aluminum alloy and a graphite epoxy plate specimen exposed to simultaneous intense heating and applied tensile loading.

Original language	English (US)
Journal	AIAA Paper
DOIs	https://doi.org/10.2514/6.1986-464
State	Published - 1986

All Science Journal Classification (ASJC) codes

General Engineering

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10.2514/6.1986-464

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title = "THERMO-MECHANICAL EFFECTS OF INTENSE THERMAL HEATING ON MATERIALS/STRUCTURES.",

abstract = "An analytical methodology for prediction of the response of metallic and composite structures subjected to combined intense heating and applied mechanical loading is presented. The proposed methodology includes a thermal analysis which incorporates nonlinear phenomena such as temperature-dependent thermophysical properties, reirradiation losses, and ablation/melting phenomena. A detailed description of a sequential, finite element, ply-by-ply failure analysis based on the maximum stress criterion is given for composite structures as well as a limit analysis approach for metallic structures. Computational projections are substantiated by experimental measurements for an aerospace aluminum alloy and a graphite epoxy plate specimen exposed to simultaneous intense heating and applied tensile loading.",

author = "Chang, {C. I.} and Griffis, {C. A.} and Stonesifer, {F. R.} and Nemes, {J. A.}",

year = "1986",

doi = "10.2514/6.1986-464",

language = "English (US)",

journal = "AIAA Paper",

issn = "0146-3705",

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T1 - THERMO-MECHANICAL EFFECTS OF INTENSE THERMAL HEATING ON MATERIALS/STRUCTURES.

AU - Chang, C. I.

AU - Griffis, C. A.

AU - Stonesifer, F. R.

AU - Nemes, J. A.

PY - 1986

Y1 - 1986

N2 - An analytical methodology for prediction of the response of metallic and composite structures subjected to combined intense heating and applied mechanical loading is presented. The proposed methodology includes a thermal analysis which incorporates nonlinear phenomena such as temperature-dependent thermophysical properties, reirradiation losses, and ablation/melting phenomena. A detailed description of a sequential, finite element, ply-by-ply failure analysis based on the maximum stress criterion is given for composite structures as well as a limit analysis approach for metallic structures. Computational projections are substantiated by experimental measurements for an aerospace aluminum alloy and a graphite epoxy plate specimen exposed to simultaneous intense heating and applied tensile loading.

AB - An analytical methodology for prediction of the response of metallic and composite structures subjected to combined intense heating and applied mechanical loading is presented. The proposed methodology includes a thermal analysis which incorporates nonlinear phenomena such as temperature-dependent thermophysical properties, reirradiation losses, and ablation/melting phenomena. A detailed description of a sequential, finite element, ply-by-ply failure analysis based on the maximum stress criterion is given for composite structures as well as a limit analysis approach for metallic structures. Computational projections are substantiated by experimental measurements for an aerospace aluminum alloy and a graphite epoxy plate specimen exposed to simultaneous intense heating and applied tensile loading.

UR - http://www.scopus.com/inward/record.url?scp=85087251980&partnerID=8YFLogxK

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U2 - 10.2514/6.1986-464

DO - 10.2514/6.1986-464

M3 - Conference article

AN - SCOPUS:85087251980

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

THERMO-MECHANICAL EFFECTS OF INTENSE THERMAL HEATING ON MATERIALS/STRUCTURES.

Abstract

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