au.\*:("WANHILL RJH")
Results 1 to 17 of 17
Selection :
MANOEUVRE SPECTRUM FATIGUE CRACK PROPAGATION IN ALUMINIUM ALLOY SHEET MATERIALSWANHILL RJH.1979; ALUMINIUM; DEU; DA. 1979; VOL. 55; NO 5; PP. 340-343; ABS. ENG/FRE; BIBL. 14 REF.Article
AQUEOUS STRESS CORROSION IN TITANIUM ALLOYSWANHILL RJH.1975; BUT. CORROS. J.; G.B.; DA. 1975; VOL. 10; NO 2; PP. 69-78; BIBL. 1 P. 1/2Article
THE EFFECT OF SHEET THICKNESS ON FLIGHT SIMULATION FATIGUE CRACK PROPAGATION IN 2024-T3, 7475-T761 AND MILL ANNEALED TI-6A1-4V.WANHILL RJH.1978; J. SOC. ENVIRONMENT. ENGRS; GBR; DA. 1978; VOL. 17; NO 2; PP. 27-32; BIBL. 24 REF.Article
FORMATION OF BRITTLE FATIGUE STRIATIONSWANHILL RJH.1975; CORROSION; U.S.A.; DA. 1975; VOL. 31; NO 2; PP. 66-71; BIBL. 29 REF.Article
CLEAVAGE OF ALUMINUM ALLOYS IN LIQUID MERCURYWANHILL RJH.1974; CORROSION; U.S.A.; DA. 1974; VOL. 30; NO 10; PP. 371-378; BIBL. 22 REF.Article
MICROSTRUCTURAL INFLUENCES ON FATIGUE AND FRACTURE RESISTANCE IN HIGH STRENGTH STRUCTURAL MATERIALS.WANHILL RJH.1978; ENGNG FRACTURE MECH.; G.B.; DA. 1978; VOL. 10; NO 2; PP. 337-357; BIBL. 4 P. 1/2Article
TITANIUM STRUCTURES IN COMMERCIAL SUBSONIC AIRCRAFTWANHILL RJH.1975; IN: INT. LEICHTMETALLTAG. 6; LEOBEN/VIENNE; 1975; DUESSELDORF; ALUMINIUM-VERLAG; DA. 1975; PP. 279-281; ABS. ALLEM. FR.; BIBL. 31 REF.Conference Paper
ENVIRONMENTAL FATIGUE CRACK PROPAGATION IN MEDIUM STRENGTH TITANIUM SHEET ALLOYSWANHILL RJH.1974; ENGNG FRACTURE MECH.; G.B.; DA. 1974; VOL. 6; NO 4; PP. 681-697; BIBL. 14 REF.Article
EFFECTS OF CRACK PLANE ORIENTATION TRANSITIONS ON FLIGHT SIMULATION FATIGUE CRACK PROPAGATION IN ALLOY 7050.WANHILL RJH; SCHRA L.1977; ALUMINIUM; DTSCH.; DA. 1977; VOL. 53; NO 7; PP. 430-433; ABS. ALLEM. FR.; BIBL. 10 REF.Article
FATIGUE FRACTURE OF ALUMINIUM ALLOY SHEET MATERIALS AT HIGH GROWTH RATES. = RUPTURE DE FATIGUE DES FEUILLES D'ALWANHILL RJH; VAN GESTEL GFJA.1976; ALUMINIUM; DTSCH.; DA. 1976; VOL. 52; NO 7; PP. 433-436; ABS. ANGL. FR.; BIBL. 13 REF.Article
THE INFLUENCE OF DIFFERENT ENVIRONMENTS ON STRESS CORROSION CRACKING OF HIGH STRENGTH ALUMINIUM ALLOY FORGINGSSCHRA L; WANHILL RJH.1983; ALUMINIUM (DUESSELD.); ISSN 0002-6689; DEU; DA. 1983-03; VOL. 59; NO 3; PP. 191-194; BIBL. 5 REF.Article
THERMOMECHANICAL TREATMENT OF ALUMINIUM ALLOYSWANHILL RJH; VENGESTEL GFJA.1978; ALUMINIUM; DEU; DA. 1978; VOL. 54; NO 9; PP. 573-580; ABS. GER/FRE; BIBL. 58 REF.Article
CADMIUM PLATING HIGH TENSILE 4340 STEELWANHILL RJH; DE RIJK P.1975; METAL FINISHG; U.S.A.; DA. 1975; VOL. 73; NO 1; PP. 32-37; BIBL. 7 REF.Article
KIC AND KISCC FOR A VERY HIGH STRENGTH TITANIUM ALLOY (IMI 551)WANHILL RJH; DE RIJK P.1974; BRIT. CORROS. J.; G.B.; DA. 1974; VOL. 9; NO 2; PP. 84-87; BIBL. 15 REF.Article
EINFLUSS VON KUGELSTRAHLEN UND BOHRUNGSAUFWEITUNG AUF DAS ERMUEDUNGSVERHALTEN VON ALZNMGCU-PROBEN = INFLUENCE DU GRENAILLAGE ET DE L'ELARGISSEMENT DES TROUS SUR LE COMPORTEMENT A LA FATIGUE DES EPROUVETTES DE ALZNMGCUDE GRAAF EAB; WANHILL RJH; DE KONING AU et al.1975; ALUMINIUM; DTSCH.; DA. 1975; VOL. 51; NO 8; PP. 514-519; BIBL. 17 REF.Article
SOME ENGINEERING PROPERTY COMPARISONS FOR 7050 AND AZ 74.61 DIE FORGINGSWANHILL RJH; SCHRA L; VAN LEEUWEN HP et al.1979; ENGNG FRACTURE MECH.; GBR; DA. 1979; VOL. 11; NO 3; PP. 507-524; BIBL. 33 REF.Article
AN AGARD-COORDINATED CORROSION FATIGUE COOPERATIVE TESTING PROGRAMME = PROGRAMME AGARD POUR LES ESSAIS DE FATIGUE AVEC CORROSIONWANHILL RJH; DE LUCCIA JJ.1982; ; FRA; DA. 1982; AGARD/R-695; 75 P.; 30 CM; ISBN 92-835-1413-0Report