Accession Number:

ADA071434

Title:

The Axial Loading Corrosion Fatigue Properties of 25 mm Thick High and Low Strength X166 Plate (DTD 5120 and DTD 5130).

Descriptive Note:

Technical rept.,

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)

Personal Author(s):

• Gunn,N. J. F.
• Ballett,J. T.

Report Date:

1978-09-01

Pagination or Media Count:

21.0

Abstract:

Axial loading fatigue tests have been made at R 0.1 in laboratory air and in a 3 12 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.

Descriptors:

• *ALUMINUM ALLOYS
• *FATIGUE(MECHANICS)
• THICKNESS
• CORROSION
• LOADS(FORCES)
• TEST METHODS
• HIGH STRENGTH
• FOG
• ENVIRONMENTAL TESTS
• METAL PLATES
• STRESS CORROSION
• LOW STRENGTH
• AXIAL FLOW
• SALT SPRAY TESTS
• UNITED KINGDOM

Subject Categories:

• Properties of Metals and Alloys
• Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE