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

Stress Intensity Distributions for Surface Flaws Under Mixed Mode Loading.

Authors: C. W. Smith; A. Andonian; w. h. peters; VIRGINIA POLYTECHNIC INST AND STATE UNIV BLACKSBURG DEPT OF ENGINEERING SCIENCE AND MECHANICS
Abstract:
Nineteen photoelastic plates, containing part circular flaws inclined at 0 deg., 30 deg. and 60 deg. to the plate surface and covering an aspect ratio range of 0.10 to 0.29 and a relative depth range of 0.20 to 0.70 were loaded parallel to the plate surfaces and analyzed by the 'frozen stress' method. Photoelastic data were fed into a digital computer programmed to provide estimates of K(1), K(2) and K(3), the stress intensity factors for loading modes I, II and III. Results revealed that: (1) For the part circular flaw shape, normalized K(1) values reveal a maximum value away from the point of maximum flaw penetration which shifts further away with increasing relative flaw depth. (2) Strong effects of inclination angle and relative depth were observed but the influence of aspect ratio in the range studied here was small. (3) K(3) effects were negligible. Results were qualitatively compared with analytical results for similar problems. (Author)

Limitations: APPROVED FOR PUBLIC RELEASE
Description: Final rept. 1 Mar 76-31 Dec 77
Pages: 48
Report Date: MAR 1978
Contract Number: F3361576C3078
Report Number: A682960
Keywords relating to this report:
*DEFECTS(MATERIALS)
*DEFECTS_MATERIALS_
*FRACTURE(MECHANICS)
*FRACTURE_MECHANICS_
*MATHEMATICAL MODELS
*PHOTOELASTICITY
*STRESS ANALYSIS
AEROSPACE SYSTEMS
AIRFRAMES
COMPUTERIZED SIMULATION
CRACKS
PLATES
SURFACES
Email This Abstract