A MIXED-MODE FRACTURE CRITERION FOR COMPOSITE MATERIALSHAHN HT.1983; COMPOSITES TECHNOLOGY REVIEW; ISSN 514683; USA; DA. 1983; VOL. 5; NO 1; PP. 26-29; BIBL. 18 REF.Article

FATIGUE BEHAVIOR AND LIFE PREDICTION OF COMPOSITE LAMINATESHAHN HT.1979; COMPOSITE MATERIALS: TESTING AND DESIGN. ASTM CONFERENCE. 5/1978/NEW ORLEANS LA; USA; PHILADELPHIA: ASTM; DA. 1979; NO 674; PP. 383-417; BIBL. 88 REF.Conference Paper

RESIDUAL STRESSES IN POLYMER MATRIX COMPOSITE LAMINATES.HAHN HT.1976; J. COMPOSITE MATER.; U.S.A.; DA. 1976-10; VOL. 10; PP. 266-278; BIBL. 19 REF.Article

ON ELASTIC-PLASTIC POISSON'S RATIO.HAHN HT.1974; J. COMPOSITE MATER.; U.S.A.; DA. 1974; VOL. 8; PP. 313-317; BIBL. 1 REF.Article

SWELLING OF COMPOSITE LAMINATESHAHN HT; KIM RY.1978; ADVANCED COMPOSITE MATERIALS-ENVIRONMENTAL EFFECTS. SYMPOSIUM ASTM. 658/1977/DAYTON OH; USA; PHILADELPHIA: ASTM; DA. 1978; PP. 98-120; BIBL. 11 REF.Conference Paper

CURING STRESSES IN COMPOSITE LAMINATES.HAHN HT; PAGANO NJ.1975; J. COMPOSITE MATER.; U.S.A.; DA. 1975; VOL. 9; NO 1; PP. 91-106; BIBL. 12 REF.Article

MECHANICAL PROPERTIES OF AN ARAMID FIBER/EPOXY COMPOSITE FOR FLYWHEEL APPLICATIONHAHN HT; CHIN WK.1982; LEADING FROM STRENGTH. SPI ANNUAL CONFERENCE. 37/1982/WASHINGTON DC; USA; NEW YORK: SPI; DA. 1982; PP. 24.C.1-24.C.6; BIBL. 4 REF.Conference Paper

INTRODUCTION TO COMPOSITE MATERIALS = INTRODUCTION AUX MATERIAUX COMPOSITESTSAI SW; HAHN HT.1980; ; USA; WESTPORT: TECHNOMIC; DA. 1980; 457 P.; 22 CM; ISBN 0-87762-288-4; 33633/691Book

LONG-TERM BEHAVIOR OF COMPOSITE MATERIALSHAHN HT; CHIAO TT.1980; ADVANCES IN COMPOSITE MATERIALS. INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS. 3/1980/PARIS; GBR; OXFORD; PARIS: PERGAMON PRESS LTD.; DA. 1980; VOL. 1; PP. 584-596; BIBL. 17 REF.; ISBN 0-08-026717-3; INTERNATIONAL SERIES ON THE STRENGTH AND FRATURE OF MATERIALS AND STRUCTURESConference Paper

FATIGUE BEHAVIOR OF COMPOSITE LAMINATE.HAHN HT; KIM RY.1976; J. COMPOSITE MATER.; U.S.A.; DA. 1976-04; VOL. 10; PP. 156-180; BIBL. 12 REF.Article

GRAPHICAL DETERMINATION OF STIFFNESS AND STRENGTH OF COMPOSITE LAMINATES.HAHN HT; TSAI SW.1974; J. COMPOSITE MATER.; U.S.A.; DA. 1974; VOL. 8; PP. 160-177; BIBL. 14 REF.Article

FAILURE CHARACTERIZATION OF A GRAPHITE/EPOXY LAMINATE THROUGH PROOF TESTINGHAHN HT; HWANG DG.1982; ASTM SPECIAL TECHNICAL PUBLICATION; ISSN 0066-0558; USA; DA. 1982; NO 787; PP. 247-273; BIBL. 23 REF.Conference Paper

EVALUATION OF COMPOSITE CURING STRESSESPAGANO NJ; HAHN HT.1977; COMPOSITE MATERIALS: TESTING AND DESIGN. ASTM CONFERENCE. 4/1976/VALLEY FORGE PA; USA; PHILADELPHIA: ASTM; DA. 1977; NO 617; PP. 317-329; BIBL. 15 REF.Conference Paper

CRACK-TYPE DAMAGE AND FRACTURE TOUGHNESS OF BORON/ALUMINIUM COMPOSITESAWERBUCH J; HAHN HT.1979; J. COMPOSITE MATER.; USA; DA. 1979-04; VOL. 13; PP. 82-107; BIBL. 31 REF.Article

STRENGTH AND ELASTIC MODULUS OF A RANDOMLY-DISTRIBUTED SHORT FIBER COMPOSITE.KNIGHT M; HAHN HT.1975; J. COMPOSITE MATER.; U.S.A.; DA. 1975; VOL. 9; NO 1; PP. 77-90; BIBL. 12 REF.Article

INDENTATION OF AN ELASTIC LAYER(S) BONDED TO A RIGID CYLINDER. I. QUASISTATIC CASE WITHOUT FRICTION.HAHN HT; LEVINSON M.1974; INTERNATION. J. MECH. SCI.; G.B.; DA. 1974; VOL. 16; NO 7; PP. 489-502; BIBL. 11 REF.Article

STRESS-RUPTURE LIFETIMES OF ORGANIC FIBER-EPOSAP STRANDS AND PRESSURE VESSELSHAHN HT; CHIE IL; GATES TL et al.1980; RISING TO THE CHALLENGE. SPI ANNUAL CONFERENCE. 35/1980/NEW ORLEANS LA; USA; NEW YORK: SPI; DA. 1980; PP. 17.D.1-17.D.7; BIBL. 17 REF.Conference Paper