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EMPIRICAL STRENGTH THEORIESSENDECKYJ GP.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 515; PP. 171-179; BIBL. 1 P. 1/2; (TEST. PREDICT. MATER. PERFORMANCE STRUCT. COMPONENTS. SYMP. I. II.; ANAHEIM, CALIF. - ATLANTIC CITY, N.J.; 1971)Conference Paper

A CLASS OF INTERFACE CRACK PROBLEMS.SENDECKYJ GP.1974; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1974; NO 560; PP. 92-104; BIBL. 11 REF.Article

EFFECT OF TIME AT LOAD ON FATIGUE RESPONSE OF ((0/ +OU- 45/90)S) T300/5208 GRAPHITE EPOXY LAMINATESENDECKYJ GP; STALNAKER HD.1977; COMPOSITE MATERIALS: TESTING AND DESIGN. ASTM CONFERENCE. 4/1976/VALLEY FORGE PA; USA; PHILADELPHIA: ASTM; DA. 1977; NO 617; PP. 39-52; BIBL. 7 REF.Conference Paper

ON THE CHANGING ORDER OF SINGULARITY AT A CRACK TIP.NUISMER RJ; SENDECKYJ GP.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 4; PP. 625-630; BIBL. 22 REF.Article

COMPARISON OF HOLOGRAPHIC, RADIOGRAPHIC, AND ULTRASONIC TECHNIQUES FOR DAMAGE DETECTION IN COMPOSITE MATERIALSSENDECKYJ GP; MADDUX GE; TRACY NA et al.1978; ICCM2. INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS/1978/TORONTO CAN; USA; WARRENDALE: AIME; DA. 1978; PP. 1037-1056; BIBL. 11 REF.Conference Paper

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