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AN EVALUATION OF THE CHEVRON V-NOTCHED BEND BAR FRACTURE TOUGHNESS SPECIMENSHIH TT.1981; ENG. FRACT. MECH.; GBR; DA. 1981; VOL. 14; NO 4; 821-829, 831-832; BIBL. 16 REF.Article

AN EVALUATION OF THE CHEVRON V-NOTCHED BEND BAR FRACTURE TOUGHNESS SPECIMENSHIH TT.1981; ENG. FRACT. MECH.; ISSN 0013-7944; USA; DA. 1981; VOL. 14; NO 4; PP. 821-832; BIBL. 16 REF.Article

AN EVALUATION OF THE PROBABILISTIC APPROACH TO BRITTLE DESIGNSHIH TT.1980; ENG. FRACT. MECH.; ISSN 0013-7944; USA; DA. 1980; VOL. 13; NO 2; PP. 257-271; BIBL. 32 REF.Article

CHEVRON V-NOTCHED BEND SPECIMEN FOR KIC MEASUREMENT OF BRITTLE MATERIALS = EPROUVETTE ENTAILLEE EN CHEVRON EN V POUR MESURE DU KIC DE MATERIAUX FRAGILESSHIH TT.1981; J. TEST. EVAL.; ISSN 0090-3973; USA; DA. 1981; VOL. 9; NO 1; PP. 50-55; BIBL. 22 REF.Article

APPLICATION OF FRACTURE MECHANICS TO CERAMIC MATERIALS. A STATE-OF-THE-ART REVIEWSHIH TT; OPOKU J.1979; ENG. FRACT. MECH.; ISSN 0013-7944; USA; DA. 1979; VOL. 12; NO 4; PP. 479-498; BIBL. 2 P.Article

EFFECT OF SPECIMEN THICKNESS ON DELAY IN FATIGUE CRACK GROWTH = INFLUENCE DE L'EPAISSEUR DE L'EPROUVETTE SUR LE RETARD A LA CROISSANCE DE LA FISSURE DE FATIGUESHIH TT; WEI RP.1975; J. TESTG EVAL.; U.S.A.; DA. 1975; VOL. 3; NO 1; PP. 46-47; BIBL. 11 REF.Article

THRESHOLD AND LOW-RATE FATIGUE CRACK GROWTH OF A NIMOV ROTOR STEELSHIH TT; DONALD JK.1981; TRANS. ASME, J. ENG. MATER. TECHNOL.; USA; DA. 1981-04; VOL. 103; NO 2; PP. 104-111; BIBL. 17 REF.Article

APPLICATION OF VELOCITY-SELECTIVE FREEZE-PUSHING TO THE SEPARATION AND CHARACTERIZATION OF AIR-BORNE SOLID PARTICULATE MATTER IN AIR POLLUTION SAMPLES = APPLICATION DE LA CONGELATION A VITESSE SELECTIVE POUR LA SEPARATION ET LA CARACTERISATION DES PARTICULES SOLIDES EN SUSPENSION DANS LES ECHANTILLONS DE CONTROLE DE LA POLLUTION ATMOSPHERIQUESHIH TT; DONAGHEY LF.sdIN: 76TH NATL. MEET. AM. INST. CHEM. ENG.; TULSA, OKLA.; 1974; NEW YORK; A.I.CH.E.; DA. S.D.; VOL. 24A; PP. 11 P; H.T. 1; BIBL. 12 REF.Conference Paper

LOW FREQUENCY FATIGUE CRACK GROWTH BEHAVIOR OF A470 CLASS 8 ROTOR STEEL AT 5380C (10000F) = ERMUEDUNGSRISSWACHSTUM BEI NIEDRIGER FREQUENZ EINES TURBINENLAEUFERSTAHLES NACH ASTM-A 470 BEI 5380C = CROISSANCE DES FISSURES DE FATIGUE A BASSE FREQUENCE DANS UN ACIER A TURBINES ASTM A 470 A 538OCSWAMINATHAN VP; SHIH TT; SAXENA A et al.1982; ENG. FRACT. MECH.; GBR; DA. 1982; VOL. 16; NO 6; 827-831, 833-836; BIBL. 17 REF.Article

ION-EXCHANGE RATES IN BIFUNCTIONAL RESINSKNAEBEL KS; COBB DD; SHIH TT et al.1979; INDUSTR. ENGNG CHEM., FUNDAM.; USA; DA. 1979; VOL. 18; NO 2; PP. 175-180; BIBL. 25 REF.Article

FATIGUE CRACK GROWTH RESPONSE FOLLOWING A HIGH-LOAD EXCURSION IN 2219-T851 ALUMINIUM ALLOY = PROPAGATION DES FISSURES DE FATIGUE DANS UN ALLIAGE D'AL 2219-T851 SOUMIS A DE HAUTES CONTRAINTESWEI RP; FENELLI NE; UNANGST KD et al.1980; J. ENG. MATER. TECHNOL.; ISSN 0094-4289; USA; DA. 1980; VOL. 102; NO 3; PP. 280-292; BIBL. 40 REF.Article

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