Accession Number:

ADA003650

Title:

Preliminary Design of Wings. Volume II. Preliminary Fatigue Design.

Descriptive Note:

Final technical rept. Feb 71-Oct 72,

Corporate Author:

FAIRCHILD REPUBLIC CO FARMINGDALE N Y

Personal Author(s):

Report Date:

1974-03-01

Pagination or Media Count:

37.0

Abstract:

This report describes an approach for obtaining ultimate tensile design allowables which should result in satisfactory fatigue performance. Thus, fatigue considerations can be included in the original design rather than being checked as an afterthought after the design has been set. This can avoid costly redesigns to obtain structural integrity in fatigue.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE