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A finite element investigation of su...

McGuire, Michael Philip.

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A finite element investigation of sustained service loads on an isogrid structure.

Record Type:	Electronic resources : Monograph/item
Title/Author:	A finite element investigation of sustained service loads on an isogrid structure./
Author:	McGuire, Michael Philip.
Description:	72 p.
Notes:	Source: Masters Abstracts International, Volume: 41-02, page: 0572.
Contained By:	Masters Abstracts International41-02.
Subject:	Engineering, Aerospace. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1410524
ISBN:	0493785752

A finite element investigation of sustained service loads on an isogrid structure.
McGuire, Michael Philip.

A finite element investigation of sustained service loads on an isogrid structure. - 72 p.

Source: Masters Abstracts International, Volume: 41-02, page: 0572.

Thesis (M.S.E.)--The University of Alabama in Huntsville, 2002.

A sample isogrid panel was studied in this research. Three different finite element MSC/NASTRAN models were used to represent the isogrid panel. The pre- and post-processing were performed using MSC/Patran.

ISBN: 0493785752Subjects--Topical Terms:

1018395
Engineering, Aerospace.

A finite element investigation of sustained service loads on an isogrid structure.
LDR:01932nmm 2200325 4500 001 1810387
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008 130610s2002 eng d
020 $a 0493785752
035 $a (UnM)AAI1410524
035 $a AAI1410524
040 $a UnM $c UnM
100 1 $a McGuire, Michael Philip. $3 1899999
245 1 0 $a A finite element investigation of sustained service loads on an isogrid structure.
300 $a 72 p.
500 $a Source: Masters Abstracts International, Volume: 41-02, page: 0572.
500 $a Adviser: Mark Bower.
502 $a Thesis (M.S.E.)--The University of Alabama in Huntsville, 2002.
520 $a A sample isogrid panel was studied in this research. Three different finite element MSC/NASTRAN models were used to represent the isogrid panel. The pre- and post-processing were performed using MSC/Patran.
520 $a The first model is a two-dimensional model employing the conventional E* and T* approximations for an isogrid panel. The second model is a three-dimensional model using two-dimensional plate elements, without the conventional approximations. The third model is a Three-dimensional solid model of the isogrid panel, also without the approximations.
520 $a In each model an attempt was made to recover the same stress information. A comparison and discussion of differences from these analyses are presented.
520 $a The results showed the conventional isogrid approximations, E* and T*, did not match the results of the other models, with the plate and solid models correlating well. The stresses found using the solid model were below the stress corrosion criteria for 7050-T7451 aluminum plate.
590 $a School code: 0278.
650 4 $a Engineering, Aerospace. $3 1018395
650 4 $a Applied Mechanics. $3 1018410
650 4 $a Engineering, Mechanical. $3 783786
690 $a 0538
690 $a 0346
690 $a 0548
710 2 0 $a The University of Alabama in Huntsville. $3 1017884
773 0 $t Masters Abstracts International $g 41-02.
790 1 0 $a Bower, Mark, $e advisor
790 $a 0278
791 $a M.S.E.
792 $a 2002
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1410524