TY  - RPRT
TI  - Thermal Inspection of a Composite Fuselage Section Using a Fixed Eigenvector Principal Component Analysis Method
AU  - Zalameda, Joseph N.
AU  - Bolduc, Sean
AU  - Harman, Rebecca
PY  - 2017
UR  - https://ntrs.nasa.gov/citations/20170004756
ID  - 20170004756
ER  -