Classical Laminate Plate Theory

Prediction of stresses and strains in a laminated plate of infinite in-plane dimensions. Allows for application of thermal and edge loads.

Launch Tool

You must login before you can run this tool.

Version 1.1 - published on 09 Oct 2014

Open source: license | download

View All Supporting Documents

Usage

Simulation Users

684 in

Zoom 1y 6m 3m

0 2 2 2 2 2 2 2 2 18 44 65 79 91 99 491 117 142 178 181 194 200 206 215 219 221 226 233 234 236 240 242 248 251 255 268 274 281 281 285 291 297 301 317 325 330 336 343 357 365 372 378 383 391 398 402 408 408 410 412 421 426 432 436 439 445 450 453 454 458 464 466 470 474 476 491 494 496 502 506 510 515 520 525 533 536 537 543 559 561 567 570 573 574 576 583 598 603 604 610 615 617 623 631 636 639 641 644 657 666 674 677 684 684
Users By Organization Type
Type Users
Unknown 627 (92.61)
Industry / Private Company 18 (2.66)
University / College Graduate Student 18 (2.66)
Government Agency 4 (0.59)
University / College Faculty 4 (0.59)
University / College Staff 3 (0.44)
National Laboratory 2 (0.3)
Military 1 (0.15)
Users by Country of Residence
Country Users
Unknown 683 (99.85%)
UNITED STATES 1 (0.15%)

Simulation Runs

6,194 in

Zoom 1y 6m 3m

0 0 0 0 0 9 9 21 25 21 235 391 710 895 1,015 1,094 1,120 1,313 2,301 2,413 2,420 2,431 2,444 2,459 2,482 2,490 2,500 2,514 2,521 2,531 2,546 2,546 2,552 2,554 2,594 2,661 2,698 2,802 2,819 2,826 2,838 2,871 2,879 2,900 2,908 2,910 2,923 2,935 3,079 3,116 3,158 3,196 3,217 3,235 3,302 3,378 3,383 3,385 3,421 3,443 3,584 3,629 3,646 3,650 3,663 3,681 3,747 3,765 3,773 3,783 3,841 3,859 3,892 3,892 3,893 3,908 3,997 4,021 4,027 4,039 4,044 4,054 4,086 4,091 4,166 4,473 4,476 4,503 4,746 4,813 4,918 5,007 5,028 5,082 5,095 5,138 5,314 5,379 5,389 5,420 5,425 5,441 5,494 5,528 5,546 5,561 5,574 5,594 5,978 6,066 6,089 6,106 6,134 6,194
Overview
Average Total
Wall Clock Time 17.3 hours 4532.92 days
CPU time 2.22 hours 581.1 days
Interaction Time 1.22 hours 319.72 days