Analyzing & Optimizing Composite Layups

Subject / Started by	Replies / Views	Last post
Grid stiffened panel optimization - question about variables? Started by HyperSizer Moderator	1 Replies 45743 Views	July 11, 2008, 03:30:55 PM by Phil
HyperSizer picks the candidate design with MAXIMUM weight. Started by iankim	3 Replies 39739 Views	September 10, 2008, 10:24:05 PM by Phil
How can I do the optimization with layup definition? Started by iankim	1 Replies 35841 Views	September 15, 2008, 10:26:45 AM by Phil
Stiffened Panel Optimization - Error Message: User Defined Analysis Undefined Started by MKLEE	1 Replies 33494 Views	October 22, 2008, 08:14:20 AM by Phil
Hard to understand the popup warning.(f06 element number) Started by iankim	1 Replies 31451 Views	October 23, 2008, 06:59:47 AM by Phil
How to switch load case Started by iankim	1 Replies 31473 Views	October 30, 2008, 10:31:25 AM by Phil
Designing with one-stack unstiffened and sandwich concepts Started by HyperSizer User	1 Replies 33940 Views	November 05, 2008, 04:15:38 PM by Phil
MOVED: Optimizing for both stiffener and frame spacing Started by Phil	0 Replies 30550 Views	November 12, 2008, 11:20:30 AM by Phil
MOVED: How do I design skins and spars with uniaxial stiffeners at once? Started by Phil	0 Replies 31702 Views	November 12, 2008, 11:21:17 AM by Phil
Hard to understand HyperSizer calculation in sandwich optimization Started by iankim	9 Replies 53088 Views	December 16, 2008, 09:01:23 AM by Phil
Correction factor for composite laminates on honeycomb core Started by HyperSizer User	4 Replies 43025 Views	June 25, 2009, 11:29:58 AM by Rocketman007
Discrete Laminates from Effective Laminates Help. Started by JEA	3 Replies 43816 Views	September 14, 2009, 07:45:08 AM by JEA
Discretization of Ply Drop Offs Started by hyperuser	1 Replies 41166 Views	April 26, 2010, 01:26:16 PM by James
PCOMP Non Structural Mass Started by garyjh	1 Replies 43272 Views	October 11, 2010, 10:16:08 AM by Phil
# Requested Designs ignored Started by cra5072	2 Replies 50694 Views	July 22, 2011, 05:49:48 PM by cra5072
Buckling margin not coinciding with FE analysis result. Started by iankim	3 Replies 55086 Views	December 21, 2012, 08:40:55 AM by Ryan
Honeycomb Core Taper Analysis Started by Mike T.	3 Replies 51545 Views	July 01, 2014, 03:50:12 PM by James
Optimizing laminates with linking groups Started by Tom Dragone	1 Replies 44566 Views	July 19, 2014, 10:22:29 AM by James
Discrepancy between ply count and thickness with effective laminates Started by Tom Dragone	1 Replies 46449 Views	July 19, 2014, 10:58:53 AM by James
Inconsistency in Load Case Results Started by Mike T.	4 Replies 49832 Views	August 08, 2014, 08:15:23 AM by Ryan