Influence of hole surface finish, cyclic frequency and spectrum severity on the fatigue behaviour of thick section aluminium alloy pin joints (U)
By: J. Y. (John Yeates) Mann, G. W. Revill and R. A. Pell.
Contributors: Pell, R. A.; Revill, G. W.; Aeronautical Research Laboratory (Australia)
Series: Aircraft structures report -- 430
Publisher: Aeronautical Research Laboratory
Published: 1987
Place of publication: Melbourne, Victoria
Number of pages: 42
Subjects: Aluminum alloys; Cracking; Fatigue tests