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Volume 44, Issue 11
1 November 1972
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 44, Issue 11
Review Article| November 01 1972

Microstructural changes that drilling and reaming can cause in the bore holes in DTD 5014 (RR58 extrusions)

P.J.E. FORSYTH, AIM
P.J.E. FORSYTH, AIM
Materials department, Royal Air Force Establishment, Farnborough.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1972
Aircraft Engineering (1972) 44 (11): 20–23.
https://doi.org/10.1108/eb034960

HOLED FATIGUE SPECIMENS, both untested and tested, were received from structures department, RAE for metallurgical examination to determine the causes of certain observed variations in total life and crack initiation time.

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© MCB UP Limited
1972
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