FATIGUE BEHAVIOR OF MATERIALS FOR THE SUPERSONIC TRANSPORT.
Abstract
The fatigue behavior of sheet materials subjected to supersonic transport load-temperature environments is being evaluated. In addition to a detailed description of the test program, this report presents extensive data obtained in constant load amplitude tests without contaminants, preliminary data on the effects of contaminants, and preliminary data obtained in evaluations of fuselage and wing root loading histories. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 31, 1964
- Accession Number
- AD0437261
Entities
People
- A. J. Mcculloch
Organizations
- Lockheed Martin