Preliminary Design of Wings. Volume II. Preliminary Fatigue Design.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1974
- Accession Number
- ADA003650
Entities
People
- Harold Switzky