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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

DEVELOPING NORMALIZED CRACK GROWTH CURVES FOR TRACKING DAMAGE IN AIRCRAFT.GALLAGHER JP; STALNAKER HD.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 114-120; BIBL. 14 REF.Article

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