TY - BOOK ID - 125043085 TI - Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure AU - Harris, Charles E. AU - Abeyounis, William Kelly AU - Langley Research Center PY - 1996 PB - Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, DB - UniCat KW - Fuselages. KW - Residual strength. KW - Crack initiation. KW - Crack propagation. KW - Fatigue (materials) KW - Computer programs. UR - https://www.unicat.be/uniCat?func=search&query=sysid:125043085 AB - ER -