Analyzing & Optimizing Composite Layups

Subject / Started by	Replies / Views	Last post
Sequecing issue Started by ChrisSummers	3 Replies 1405 Views	October 18, 2019, 03:39:23 AM by ChrisSummers
Linking layups for PORT/STBD components in linking groups Started by ChrisSummers	3 Replies 512 Views	October 08, 2019, 11:30:38 AM by Brent
Error Message - Set Variables for component/Assembly, number of laminates Started by martinjb	0 Replies 10693 Views	June 12, 2017, 10:41:18 AM by martinjb
Database Issues Started by Stressed	1 Replies 3949 Views	February 16, 2017, 08:50:45 AM by James
Way to Define Composite Ply Angle Tolerance? Started by khender	1 Replies 3243 Views	October 24, 2016, 09:43:42 AM by James
how to resize a single component by passing from DL to EL ? Started by eugenio	1 Replies 3803 Views	November 23, 2015, 08:42:02 AM by Brent
Regarding wind turbine blade (cutting components) Started by orchidworld	2 Replies 4661 Views	April 08, 2015, 10:35:43 PM by orchidworld
+/-30* plies Started by eric	5 Replies 5576 Views	March 20, 2015, 09:25:45 AM by James
Inconsistency in Load Case Results Started by Mike T.	4 Replies 4951 Views	August 08, 2014, 08:15:23 AM by Ryan
Discrepancy between ply count and thickness with effective laminates Started by Tom Dragone	1 Replies 4409 Views	July 19, 2014, 10:58:53 AM by James
Optimizing laminates with linking groups Started by Tom Dragone	1 Replies 4339 Views	July 19, 2014, 10:22:29 AM by James
Honeycomb Core Taper Analysis Started by Mike T.	3 Replies 6276 Views	July 01, 2014, 03:50:12 PM by James
Buckling margin not coinciding with FE analysis result. Started by iankim	3 Replies 9369 Views	December 21, 2012, 08:40:55 AM by Ryan
# Requested Designs ignored Started by cra5072	2 Replies 9279 Views	July 22, 2011, 05:49:48 PM by cra5072
PCOMP Non Structural Mass Started by garyjh	1 Replies 8284 Views	October 11, 2010, 10:16:08 AM by Phil
Discretization of Ply Drop Offs Started by hyperuser	1 Replies 7996 Views	April 26, 2010, 01:26:16 PM by James
Discrete Laminates from Effective Laminates Help. Started by JEA	3 Replies 9013 Views	September 14, 2009, 07:45:08 AM by JEA
Correction factor for composite laminates on honeycomb core Started by HyperSizer User	4 Replies 12867 Views	June 25, 2009, 11:29:58 AM by Rocketman007
Hard to understand HyperSizer calculation in sandwich optimization Started by iankim	9 Replies 14436 Views	December 16, 2008, 09:01:23 AM by Phil
MOVED: How do I design skins and spars with uniaxial stiffeners at once? Started by Phil	0 Replies 7837 Views	November 12, 2008, 11:21:17 AM by Phil