Conditions for Symmetries in the Buckle Patterns of Laminated-Composite Plates

By: Administration (Nasa), National Aeronaut

Technical Report Nemeth, Michael P. Langley Research Center NASA/TM-2012-217589, L-20159, NF1676L-14994 WBS 869021.04.07.01.13 BUCKLING; PLATES (STRUCTURAL MEMBERS); LAMINATES; SYMMETRY; THICKNESS; INVARIANCE; EIGENVALUES

• Format: Paperback
• Language: English
• ISBN: B08F6RC8TX
• ISBN13: 9798672858654
• Release Date: January 1
• Publisher: Independently Published
• Length: 46 Pages
• Weight: 0.29 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"