au.\*:("CHANANI GR")
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RETARDATION OF FATIGUE-CRACK GROWTH IN 7075 ALUMINIUM = RETARD A LA CROISSANCE DES FISSURES DE FATIGUE DANS L'ALUMINIUM 7075CHANANI GR.1975; METALS ENGNG QUART.; U.S.A.; DA. 1975; VOL. 15; NO 1; PP. 40-48; BIBL. 23 REF.Article
OBSERVATION OF CRACKS-CLOSURE BEHAVIOR AFTER SINGLE OVERLOAD CYCLES IN 7075-T6 SINGLE-EDGE-NOTCHED SPECIMENS.CHANANI GR; MAYS BJ.1977; ENGNG FRACTURE MECH.; G.B.; DA. 1977; VOL. 9; NO 1; PP. 65-73; BIBL. 18 REF.Article
FATIGUE CRACK PROPAGATION IN TRIP STEELSCHANANI GR; ANTOLOVICH SD; GERBERICH WW et al.1972; METALLURG. TRANS.; U.S.A.; DA. 1972; VOL. 3; NO 10; PP. 2661-2672; BIBL. 41 REF.Serial Issue
FRACTURE TOUGHNESS OF DUPLEX STRUCTURES. II. LAMINATES IN THE DIVIDER ORIENTATIONANTOLOVICH SD; KASI K; CHANANI GR et al.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 514; PP. 135-150; BIBL. 20 REF.; (FRACT. THOUGHNESS. PROC. 1971 NATL. SYMP. FRACT. MECH.; URBANA-CHAMPAIGN, ILL.; 1971)Conference Paper
FRACTURE TOUGHNESS OF DUPLEX STRUCTURES. I. TOUGH FIBERS IN A BRITTLE MATRIXANTOLOVICH SD; SHETE PM; CHANANI GR et al.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 514; PP. 114-134; BIBL. 17 REF.; (FRACT. THOUGHNESS. PROC. 1971 NATL. SYMP. FRACT. MECH.; URBANA-CHAMPAIGN, ILL.; 1971)Conference Paper
A MODEL FOR FATIGUE CRACK PROPAGATION. = UN MODELE POUR LA PROPAGATION DE FISSURE EN FATIGUEANTOLOVICH SD; SAXENA A; CHANANI GR et al.1975; ENGNG FRACTURE MECH.; G.B.; DA. 1975; VOL. 7; NO 4; PP. 649-652; BIBL. 18 REF.Article
FRACTURE MECHANISM TRANSITIONS IN LAMINATE COMPOSITESANTOLOVICH SD; CHANANI GR; SAXENA A et al.1973; J. PHYS. D; G.B.; DA. 1973; VOL. 6; NO 5; PP. 560-571; BIBL. 17 REF.Serial Issue