The effect of fatigue crack length on the residual strength of ARALL3 panels with fingertip doublers
By: W. van der Hoeven.
Contributors: National Aerospace Laboratory (The Netherlands)
Publisher: National Aerospace Laboratory
Published: 1994
Place of publication: Amsterdam
Number of pages: 38
Subjects: Aluminum alloys; Crack propagation; Fatigue
Notes: Bibliographical references: p. 22.