References
- [1] Tomblin, J.S., Lacy, T., Smith, B., Hooper, S., Vizzini, A., Lee, S., Review of Damage Tolerance for Composite Sandwich Airframe Structures, Final Report, DOT/FAA/AR-99/49, 1999.
- [2] CMH-17, Composite Materials Handbook, Volume 1. Polymer Matrix Composites Guidelines for Characterization of Structural Materials. SAE International, 2012.
- [3] Tomblin J.S., Senevirante W. P., Durability And Damage Tolerance Testing of a Beechcraft Starship Forward-Wing With Large Damages, Final Report, DOT/FAA/TC-13/26, 2017.
- [4] Adams D. O., Kuramoto B., Damage tolerance test method development for sandwich composites.
- [5] Gang Z., Leung H., Zheng C., Robinson B., New four-point bending based method for impact damage tolerance assessment of sandwich structure, Chinese Society for Composite Materials, 2017.
- [6] ASTM standard D7249/D7249M, Standard Test Method for Facesheet Properties of Sandwich Constructions by Long Beam Flexure, ASTM International, 2018.
- [7] European Aviation Safety Agency, 2010, AMC 20-29 Composite Aircraft Structure.
- [8] ASTM standard ASTM D7137/D7137M, Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates, ASTM International, 2017.