1. The FAA and Industry Guide to Product Certification, 2004. Second Edition, prepared by AIA, GAMA, and the FAA Aircraft Certification Service, September.
2. AIR100-2010-120-003, 2010. Acceptance of Composite Specification and Design Values Developed using the NCAMP Process, September 20.
3. Ilcewicz, L.B., Ashforth, C.A., 2017. Scaling Crucial to Integrated Product Development of Composite Airframe Structures, current volume.
4. Whitehead, R.S., Kan, H.P., Cordero, R., Saether, E.S., 1986. Certification testing methodology for composite structures, Report No. NADC-87042-60, Volumes I and II.
5. Seneviratne, W.P., Tomblin, J.S., 2011. Fatigue test data for composite design variables, with & without damage. In: 2011 FAA/EASA/Industry Composite Transport Fatigue, Damage Tolerance, Maintenance & Crashworthiness Workshop, Atlanta, GA.