Turbine engine rotor blade containment/durability.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, [1990]
Series:	Advisory circular ; AC no. 33-5
Subjects:	Airplanes > Turbine-propeller engines > Design and construction. Airplanes > Turbojet engines > Blades.
Online Access:	https://purl.fdlp.gov/GPO/LPS106292

Available Online