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Composite Laminate Analysis

By Andrew Ritchey

Purdue University

Uses basic laminate theory to estimate effective laminate properties and residual stresses, strains and deformations due to thermal loading.

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Version 1.2 - published on 12 Apr 2010

doi:10.4231/D3QV3C37P cite this

Open source: license | code unavaialble

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Usage

World usage

Location of all "Composite Laminate Analysis" Users Since Its Posting

Simulation Users

111

2 17 20 21 22 26 29 32 35 37 38 40 42 43 63 66 66 66 69 71 71 75 78 80 82 84 91 94 95 95 96 98 100 103 105 105 105 106 107 110 111

Users By Organization Type
Type Users
Educational - University 97 (87.39%)
Unidentified 8 (7.21%)
Industry 4 (3.6%)
Military 1 (0.9%)
National Lab 1 (0.9%)
Users by Country of Residence
Country Users
us UNITED STATES 73 (76.04%)
in INDIA 8 (8.33%)
co COLOMBIA 3 (3.13%)
it ITALY 2 (2.08%)
br BRAZIL 2 (2.08%)
tr TURKEY 2 (2.08%)
ca CANADA 2 (2.08%)
tw TAIWAN 2 (2.08%)
ch SWITZERLAND 1 (1.04%)
gb UNITED KINGDOM 1 (1.04%)

Simulation Runs

1,367

27 146 172 253 264 275 291 306 331 337 338 342 351 356 668 705 708 717 745 776 789 816 847 860 867 871 934 948 961 969 1060 1150 1155 1251 1271 1271 1279 1289 1309 1356 1367
Overview
Average Total
Wall Clock Time 2.34 hours 75.5 days
CPU time 0.77 seconds 9.92 minutes
Interaction Time 55.65 minutes 29.95 days

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