TY  - RPRT
TI  - An Analysis Methodology to Predict Damage Propagation in Notched Composite Fuselage Structures
AU  - Bergan, A.
AU  - Davila, C.
AU  - Leone, F.
AU  - Awerbuch, J.
AU  - Tan, T.-M.
PY  - 2015
UR  - https://ntrs.nasa.gov/citations/20160007429
ID  - 20160007429
ER  -