FN Archimer Export Format PT J TI Comparison of test configurations for determination of mode II interlaminar fracture toughness results from international collaborative test programme BT AF DAVIES, Peter SIMS, GD BLACKMAN, BRK BRUNNER, AJ KAGEYAMA, K HOJO, M TANAKA, K MURRI, G ROUSSEAU, C. GIESEKE, B MARTIN, RH AS 1:1;2:2;3:3;4:4;5:5;6:6;7:7;8:8;9:9;10:10;11:11; FF 1:;2:;3:;4:;5:;6:;7:;8:;9:;10:;11:; C1 IFREMER, Ctr Brest, Technopole Brest Iroise, F-29280 Plouzane, France. Natl Phys Lab, Teddington, Middx, England. Univ London Imperial Coll Sci Technol & Med, London, England. Eidgenossische Mat Prufungs & Forschungsanhalt, Dubendorf, Switzerland. Univ Tokyo, Tokyo, Japan. Kyoto Univ, Kyoto, Japan. Toyama Prefectural Univ, Toyama, Japan. NASA, Hampton, VA USA. Bell Helicopters, Ft Worth, TX USA. Cincinnati Testing Labs, Cincinnati, OH USA. Mat Engn Res Lab Ltd, Hertford, England. C2 IFREMER, FRANCE NPL, UK IMPERIAL COLL LONDON, UK EMPA, SWITZERLAND UNIV TOKYO, JAPAN UNIV KYOTO, JAPAN UNIV TOYAMA, JAPAN NASA, USA BELL HELICOPTERS, USA CINTESTLABS, USA MERL, UK SI BREST IF 0.174 TC 85 UR https://archimer.ifremer.fr/doc/00148/25883/24089.pdf LA English DT Article DE ;Delamination;Fracture tests;Mode II;Interlaminar shear;Fracture toughness AB This paper presents a summary of the tests performed within a Versailles Project on Advanced Materials and Standards collaborative test programme to examine the measurement of mode II interlaminar fracture toughness using four different test methods based on end notched flexure, stabilised end notched flexure, end loaded split, and four point end notched flexure carbon fibre reinforced epoxy specimens. Tests were performed by members of the European Structural Integrity Society, the Japan Industrial Standards group, and the American Society for Testing and Materials. PRC/1546 PY 1999 SO Plastics Rubber And Composites SN 1465-8011 PU Maney Publishing VL 28 IS 9 UT 000085061600005 BP 432 EP 437 DI 10.1179/146580199101540600 ID 25883 ER EF