1. Federal aviation regulation part 33, section 33.94-blade containment and rotor unbalance tests;Federal Aviation Administration (United States),1984
2. Defense standard 00-971—general specification for aircraft gas turbine engines;Ministry of Defense (United Kingdom),1987
3. CCAR-33 – airworthiness standards: aircraft engines;Civil Aviation Administration of China,2005
4. Effects of multiple blade interaction on the containment of blade fragments during a rotor failure;Sarkar;Finite Elem. Anal. Des.,1996
5. Aircraft engine blade-out dynamics;Carney,2002