Fatigue Substantiation Procedures for General Aviation Aircraft Structures

Format:

Conference/Event

Author/Creator:

Anderjaska, Arnold E., author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1971-03-24 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1971

Summary:

Fatigue substantiation of wing structure on small airplanes is now required by the Federal Aviation Regulations for civil type certification of new designs. Methods for substantiation of this structure under the "safe-life" concept, including suggested loading spectra and procedures for strength determination are outlined. The background leading to these methods and a basis for establishing scatter factors are presented. Procedures for substantiation under the "fail-safe" concept are also given

Notes:

Vendor supplied data

Publisher Number:

710404

Access Restriction:

Restricted for use by site license