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au.\*:("RADHAKRISHNAN VM")

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PARAMETER REPRESENTATION OF FATIGUE CRACK GROWTHRADHAKRISHNAN VM.1979; ENGNG FRACTURE MECH.; GBR; DA. 1979; VOL. 11; NO 2; PP. 359-372; BIBL. 15 REF.Article

CREEP DEFORMATION OF COPPER IN BENDINGRADHAKRISHNAN VM.1972; SCRIPTA METALLURG.; E.U.; DA. 1972; VOL. 6; NO 9; PP. 827-832; BIBL. 6 REF.Serial Issue

STRAIN RANGE PARTITIONING METHOD FOR THE ANALYSIS OF CREEP FATIGUE BEHAVIOUR OF MATERIALSRADHAKRISHNAN VM.1980; J. SCI. IND. RES.; ISSN 0022-4456; IND; DA. 1980; VOL. 39; NO 1; PP. 21-27; BIBL. 9 REF.Article

CUMULATIVE DAMAGE IN CREEPRADHAKRISHNAN VM.1979; ENGNG FRACTURE MECH.; GBR; DA. 1979; VOL. 11; NO 2; PP. 373-383; BIBL. 16 REF.Article

ON STRESS RATCHETTING. = DU "RATCHETTING" DES CONTRAINTESRADHAKRISHNAN VM.1975; J. APPL. MECH.; U.S.A.; DA. 1975; VOL. 42; NO 4; PP. 884-886; BIBL. 4 REF.Article

CREEP RUPTURE UNDER CYCLIC STRESSINGRADHAKRISHNAN VM.1973; INDIAN J. TECHNOL.; INDIA; DA. 1973; VOL. 2; NO 12; PP. 728-731; BIBL. 11 REF.Article

EFFECT OF POROSITY ON MECHANICAL PROPERTIES OF ALUMINIUM ALLOY CASTINGS: COMMENTS I = INFLUENCE DE LA POROSITE SUR LES CARACTERISTIQUES MECANIQUES DES PIECES MOULEES EN ALLIAGES D'ALUMINIUM. COMMENTAIRE IRADHAKRISHNAN VM.1982; TRANSACTIONS OF THE INDIAN INSTITUTE OF METALS; ISSN 0019-493X; IND; DA. 1982; VOL. 35; NO 3; PP. 295-296; BIBL. 1 REF.Article

CUMULATIVE DAMAGE IN LOW-CYCLE FATIGUERADHAKRISHNAN VM.1978; EXPER. MECH.; USA; DA. 1978; VOL. 18; NO 8; PP. 292-296; BIBL. 8 REF.Article

FATIGUE HARDENING AND FAILURE OF COPPER AT INTERMEDIATE LIFE.RADHAKRISHNAN VM.1977; TRANS. JAP. INST. METALS; JAP.; DA. 1977; VOL. 18; NO 3; PP. 144-148; BIBL. 11 REF.Article

EFFECT OF NOTCH IN STATIC & DYNAMIC STRESSINGRADHAKRISHNAN VM.1974; INDIAN J. TECHNOL.; INDIA; DA. 1974; VOL. 12; NO 2; PP. 43-47; BIBL. 6 REF.Article

A PARAMETRIC APPROACH TO CYCLIC CREEP.RADHAKRISHNAN VM.1976; J. APPL. MECH.; U.S.A.; DA. 1976; VOL. 43; NO 1; PP. 28-32; BIBL. 15 REF.Article

STRESS RATCHETTING UNDER TENSION AND CYCLIC TORSION. = ACCUMULATION DE CONTRAINTE SOUS TRACTION ET TORSION CYCLIQUERADHAKRISHNAN VM.1975; NUCL. ENGNG DESIGN; NETHERL.; DA. 1975; VOL. 34; NO 3; PP. 379-387; BIBL. 8 REF.Article

QUANTIFYING THE PARAMETERS IN FATIGUE CRACK PROPAGATIONRADHAKRISHNAN VM.1980; ENG. FRACT. MECH.; ISSN 0013-7944; USA; DA. 1980; VOL. 13; NO 1; PP. 129-141; BIBL. 18 REF.Article

EFFECT OF MEAN STRESS IN HIGH-TEMPERATURE FATIGUE.RADHAKRISHNAN VM.1978; EXPER. MECH.; U.S.A.; DA. 1978; VOL. 18; NO 5; PP. 196-200; BIBL. 13 REF.Article

ON NON-PROPAGATING FATIGUE CRACKS = SUR LES FISSURES DE FATIGUE NE SE PROPAGEANT PASRADHAKRISHNAN VM.1975; MATERIALPRUEFUNG; DTSCH.; DA. 1975; VOL. 17; NO 9; PP. 313-316; ABS. ALLEM. FR.; BIBL. 11 REF.Article

EFFECT OF STRESS CHANGE ON CREEP DEFORMATION.RADHAKRISHNAN VM.1973; INDIAN J. TECHNOL.; INDIA; DA. 1973; VOL. 11; NO 4; PP. 160-163; BIBL. 8 REF.Article

AN ANALYSIS OF GRAIN SIZE AND YIELD STRESS EFFECTS ON STRESS AT FATIGUE LIMIT AND THRESHOLD STRESS INTENSITY FACTORMUTOH Y; RADHAKRISHNAN VM.1981; J. ENG. MATER. TECHNOL.; ISSN 0094-4289; USA; DA. 1981; VOL. 103; NO 3; PP. 229-233; BIBL. 23 REF.Article

AN INVESTIGATION OF ROLLING FATIGUE FAILURE IN LOW ALLOY STEEL.RADHAKRISHNAN VM; RAMANATHAN S.1976; TRANS. IRON STEEL INST. JAP.; JAP.; DA. 1976; VOL. 16; NO 7; PP. 368-373; BIBL. 12 REF.Article

HIGH TEMPERATURE DEFORMATION OF ALUMINIUM UNDER UNSTEADY LOAD = DEFORMATION A HAUTE TEMPERATURE DE L'ALUMINIUM SOUS CHARGE VARIABLERADHAKRISHNAN VM; PATHAK SD.1975; ALUMINIUM; DTSCH.; DA. 1975; VOL. 51; NO 5; PP. 346-349; ABS. ALLEM. FR.; BIBL. 16 REF.Article

HIGH TEMPERATURE FATIGUERADHAKRISHNAN VM; RAGHAVAN KS.1973; INDIAN J. TECHNOL.; INDIA; DA. 1973; VOL. 2; NO 12; PP. 724-727; BIBL. 7 REF.Article

AN ANALYSIS OF GRAIN SIZE AND YIELD STRESS EFFECTS ON STRESS AT FATIGUE LIMIT AND THRESHOLD STRESS INTENSITY FACTORMUTOH Y; RADHAKRISHNAN VM.1981; TRANS. ASME, J. ENG. MATER. TECHNOL.; USA; DA. 1981-07; VOL. 103; NO 3; PP. 229-233; BIBL. 23 REF.Article

EFFECT OF TEMPERATURE ON CREEP CRACK GROWTHRADHAKRISHNAN VM; MCEVILY AJ.1980; J. ENG. MATER. TECHNOL.; ISSN 0094-4289; USA; DA. 1980; VOL. 102; NO 4; PP. 350-355; BIBL. 14 REF.Article

MECHANISM OF DEFORMATION AND FAILURE OF ALUMINIUM IN ROLLING CONTACT FATIGUERADHAKRISHNAN VM; RAMANATHAN S.1975; ALUMINIUM; DTSCH.; DA. 1975; VOL. 51; NO 7; PP. 462-467; ABS. ALLEM. FR.; BIBL. 12 REF.Article

AN INVESTIGATION OF THE EFFECT OF PRE-STRAINING ON FATIGUE CRACK GROWTHRADHAKRISHNAN VM; BABURAMANI PS.1975; MATER. SCI. ENGNG; NETHERL.; DA. 1975; VOL. 17; NO 2; PP. 283-288; BIBL. 21 REF.Article

TIME DEPENDENT CRACK GROWTH IN A TITANIUM ALLOY = PROPAGATION DES FISSURES EN FONCTION DU TEMPS DANS UN ALLIAGE DE TITANERADHAKRISHNAN VM; MCEVILY AJ.1981; SCR. METALL.; ISSN 0036-9748; USA; DA. 1981; VOL. 15; NO 1; PP. 51-54; BIBL. 11 REF.Article

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