HAMILTON'S LAW APPLIED TO THE NON-STATIONARY ELASTODYNAMICS OF PLATESBAILEY CD.1982; MECHANICS RESEARCH COMMUNICATIONS; ISSN 0093-6413; USA; DA. 1982; VOL. 9; NO 6; PP. 381-389; BIBL. 21 REF.Article

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EXACT AND DIRECT ANALYTICAL SOLUTIONS TO VIBRATING SYSTEMS WITH DISCONTINUITIESBAILEY CD.1978; J. SOUND VIBR.; GBR; DA. 1978; VOL. 60; NO 4; PP. 607Article

COMMENT ON "FINITE ELEMENTS FOR INITIAL VALUE PROBLEMS IN DYNAMICS"BAILEY CD.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 159-160; BIBL. 15 REF.Article

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APPLICATION OF HAMILTON'S LAW TO FORCED, DAMPED, STATIONARY STYSTEMSBAILEY CD.1981; J. SOUND VIB.; ISSN 0022-460X; GBR; DA. 1981; VOL. 75; NO 1; PP. 117-126; BIBL. 24 REF.Article

THE GALERKIN FORMULATION AND THE HAMILTON-RITZ FORMULATION: A COMPARISONBAILEY CD.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 44-48; BIBL. 27 REF.Conference Paper

DIRECT ANALYTICAL SOLUTIONS TO NON-UNIFORM BEAM PROBLEMS.BAILEY CD.1978; J. SOUND VIBR.; G.B.; DA. 1978; VOL. 56; NO 4; PP. 501-507; BIBL. 13 REF.Article

ON A MORE PRECISE STATEMENT OF HAMILTON'S PRINCIPLEBAILEY CD.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 30-36; BIBL. 13 REF.Conference Paper

APPLICATION OF HAMILTON'S LAW OF VARYING ACTION. = APPLICATION DE LA LOI D'ACTION VARIABLE D'HAMILTONBAILEY CD.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 9; PP. 1154-1157; BIBL. 8 REF.Article

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COMMENT ON "A DIRECT METHOD FOR ANALYSING THE FORCED VIBRATIONS OF CONTINUOUS SYSTEMS HAVING DAMPINGBAILEY CD; LEISSA AW.1979; J. SOUND VIBR.; GBR; DA. 1979; VOL. 66; NO 4; PP. 615-620; BIBL. 27 REF.Article

ACOUSTIC EMISSION: AN EMERGING TECHNOLOGY FOR ASSESSING FATIGUE DAMAGE IN AIRCRAFT STRUCTUREBAILEY CD; PLESS WM.1981; MATER. EVAL.; ISSN 0025-5327; USA; DA. 1981; VOL. 39; NO 11; PP. 1045-1060; BIBL. 12 REF.Article

COMMENT ON "HAMILTON'S LAW AND THE STABILITY OF NONCONSERVATIVE CONTINUOUS SYSTEM"SMITH CV JR; BAILEY CD.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 3; PP. 415-416; BIBL. 22 REF.Article

ACOUSTIC EMISSION OF IMPACT-DAMAGED GRAPHITE-EPOXY COMPOSITESBAILEY CD; HAMILTON JM JR; PLESS WM et al.1979; MATER. EVALUAT.; USA; DA. 1979; VOL. 37; NO 6; PP. 43-54; (7 P.); BIBL. 13 REF.Article

ACOUSTIC EMISSION DETECTION OF FATIGUE CRACK GROWTH IN A PRODUCTION-SIZE AIRCRAFT WING TEST ARTICLE UNDER SIMULTATED FLIGHT LOADS. = DETECTION PAR EMISSION ACOUSTIQUE DE LA PROPAGATION DES FISSURES PAR FATIGUE DANS UNE AILE D'AVION GRANDEUR REELLE SOUMIS A DES CHARGES DE VOL SIMULEESPLESS WM; BAILEY CD; HAMILTON JM et al.1978; MATER. EVALUAT.; U.S.A.; DA. 1978; VOL. 36; NO 5; PP. 41-48; BIBL. 10 REF.Article

ACOUST. EMISSION MONITORS DAMAGE PROGRESSION IN GRAPHITE EPOXY COMPOSITE STRUCTUREBAILEY CD; FREEMAN SM; HAMILTON JM JR et al.1980; MATER. EVAL.; ISSN 0025-5327; USA; DA. 1980; VOL. 38; NO 8; PP. 21-27; BIBL. 11 REF.Article

AE MONITORING OF RAPID CRACK GROWTH IN A PRODUCTION-SIZE WING FATIGUE TEST ARTICLE.BAILEY CD; HAMILTON JM; PLESS WM et al.1976; N.D.T. INTERNATION.; G.B.; DA. 1976; VOL. 9; NO 6; PP. 298-304; BIBL. 7 REF.Article