TY - BOOK ID - 146042293 TI - Methodology for predicting the onset of widespread fatigue damage in lap-splice joints AU - Newman, J. C. AU - Langley Research Center PY - 1998 PB - Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, DB - UniCat KW - Crack propagation. KW - Crack tips. KW - Airframes. KW - Stress analysis. KW - Lap joints. KW - Fuselages. KW - Finite element method. KW - Fatigue tests. KW - Fatigue (materials) UR - https://www.unicat.be/uniCat?func=search&query=sysid:146042293 AB - ER -