Fatigue Crack Growth in Laser Shock Peened Ti-6AL-4V Aerofoils Subjected to Foreign Object Damage
Conference; 53rd, AIAA/ASME/ASME/ASCE/AHS/ASC Structures, structural dynamics and materials ; 2012 ; Honolulu, HI
2012-01-01
11 pages
Includes bibliographical references and author index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2011
|High cycle fatigue limit stresses for airfoils subjected to foreign object damage
Tema Archive | 2003
|