TY - BOOK ID - 146066482 TI - A progressive damage methodology for residual strength predictions of notched composite panels AU - Coats, Timothy W. AU - Harris, Charles E. AU - Langley Research Center PY - 1998 PB - Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, DB - UniCat KW - Composite structures. KW - Crack propagation. KW - Epoxy matrix composites. KW - Fractography. KW - Fracture mechanics. KW - Fracture strength. KW - Laminates. KW - Loads (forces) KW - Residual strength. UR - https://www.unicat.be/uniCat?func=search&query=sysid:146066482 AB - ER -