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A methodology for computing nonlinear fracture parameters for a bulging crack in a pressurised aircraft fuselage
V. B. Shenoy, D. O. Potyondy, S. N. AtluriVolume:
14
Language:
english
Pages:
20
Journal:
Computational Mechanics
DOI:
10.1007/bf00350836
Date:
September, 1994
File:
PDF, 2.42 MB
english, 1994