(Received 10 April 2008; accepted 13 June 2008)
Published Online: 22 July 2008
CODEN: JAIOAD
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Advanced surface treatment methods for imparting beneficial residual compressive stresses into fatigue-prone metallic components such as laser shock processing (LSP) and low plasticity burnishing (LPB) have proven highly effective in prolonging the life of titanium turbine engine blades. The objective of the current effort was to experimentally evaluate whether similar life enhancement benefits are possible for metallic aircraft structures. Under this initiative, aluminum test specimens were processed using three engineered residual stress techniques, referred to as LSP 1, LSP 2, and LPB, and subsequently fatigue tested under uniaxial, constant amplitude loading conditions. Evaluation of the test results indicated that both the LSP and LPB processes, if carefully designed and applied, have the potential to increase the fatigue life of aircraft structural components.
Author Information:
Langer, Kristina
Air Force Research Laboratory, Air Vehicles Directorate, Wright-Patterson Air Force Base, OH
VanHoogen, Scott
Hoover, Jeffery
Stock #: JAI101661
ISSN:1546-962X
DOI: 10.1520/JAI101661
Author