The Axial Loading Corrosion Fatigue Properties of 25 mm Thick High and Low Strength X166 Plate (DTD 5120 and DTD 5130).
Abstract
Axial loading fatigue tests have been made at R = 0.1 in laboratory air and in a 3 1/2% NaCl fog using holed transverse sheet type test pieces (KT = 2.52) cut from the mid-section position of 25mm thick, high and low strength X166 plates to DTD 5120 and DTD 5130.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1978
- Accession Number
- ADA071434
Entities
People
- J. T. Ballett
- N. J. F. Gunn
Organizations
- Royal Aircraft Establishment