Guidance material for fatigue limit tests and composite blade fatigue substantiation.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001]
Series:	Advisory circular ; AC no. 35.37-1A
Subjects:	Propellers, Aerial > Fatigue > Testing.
Online Access:	https://purl.fdlp.gov/GPO/LPS106486

Available Online