Storming Media: Pentagon Reports and DocumentsPentagon Reports: Fast. Definitive. Complete.     
New Account »
Forgot Password?
Advanced Search »
AviationAircraft

The Effects of LCF Loadings on HCF Crack Growth

Authors: R. F. Hall; B. E. Powell; J. Byrne; PORTSMOUTH UNIV (UNITED KINGDOM) DEPT OF MECHANICAL AND MANUFACTURING ENGINEERING
Abstract:
This report results from a contract tasking University of Portsmouth as follows: The contractor will investigate high cycle fatigue (HCF) effects in structural materials. This work will be a logical follow-on to three previous phases conducted under EOARD contract. In this phase, the contractor will: (1) extend the study of the effect of prior overloads by the employment of larger overload ratios; (2) establish the conditions at which the effects of overloads in the HCF + LCF loadings completely suppress the damage caused by HCF cycles; and (3) extend the analysis of new models to overcome the shortcomings of the Wheeler model to predict the onset of HCF cycle damage.

Limitations: APPROVED FOR PUBLIC RELEASE
Description: Final rept. 22 Sep 2000-22 Nov 2001, Phase 4
Pages: 36
Report Date: FEB 2002
Contract Number: F61775-00-WE041
Report Number: A469104
Keywords relating to this report:
*CRACK PROPAGATION
*OVERLOAD
AEROSPACE SYSTEMS
AGING_MATERIALS_
AIRCRAFT ENGINES
CORROSION
CRACKING_FRACTURING_
CYCLIC RATE
FATIGUE_MECHANICS_
FRETTING
LIFE CYCLE TESTING
NONDESTRUCTIVE TESTING
OPERATIONAL READINESS
PROPULSION SYSTEMS
STRUCTURAL MECHANICS
TITANIUM ALLOYS
UNITED KINGDOM
Email This Abstract