1. Federal Aviation Administration. Advisory Circular 33.14-1. Damage tolerance for high energy turbine engine rotors. U. S. Department of Transportation, FAA, Washington, DC (2001)
2. Federal Aviation Administration. Advisory Circular 33.70-1. Guidance material for aircraft engine-life-limited parts requirements. U. S. Department of Transportation, FAA, Washington, DC (2009)
3. Federal Aviation Administration. Advisory Circular 33.70-2. Damage tolerance of hole features in high-energy turbine engine rotors. U. S. Department of Transportation, FAA, Washington, DC (2009)
4. Federal Aviation Administration. Turbine rotor material design. Federal Aviation Administration, Washington, D.C. (2000). Report No.1: DOT/FAA/AR-00/64
5. Ding, S.T., Zhou, H.M., Pan, B.C., et al.: An experimental method to obtain the hard alpha anomaly distribution for titanium alloy aeroengine disks. Chin. J. Aeronaut. (2020)