1. Fatigue, fail safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic and commuter category airplanes, Advisory Circular Federal Aviation Administration, FAA - AC 23–13A
2. The Effect of Loading Parameters on Fatigue of Composite Laminates: Part III, U.S. Department of Transportation – Federal Aviation Administration, Report DOT/FAA/AR-99/22, June 1999
3. The Effect of Loading Parameters on Fatigue of Composite Laminates: Part V, U.S. Department of Transportation – Federal Aviation Administration, Report DOT/FAA/AR-01/24, June 2001
4. Kudva, J.N., Grage, M.J., Roberts, M.M.: Aircraft structural health monitoring and other smart structures technologies – perspectives on development of smart aircraft. In: Proceedings of the 2nd International Workshop on Structural Health Monitoring (ed. F.-K. Chang), Stanford, California, pp. 122–132 (1999)
5. Kudva, J.N.: Overview of the DARPA smart wing project. J. Intell. Mater. Syst. Struct. 15, 261–267 (2004)