THE GALERKIN FORMULATION AND THE HAMILTON-RITZ FORMULATION: A COMPARISONBAILEY CD.1980; ACTA MECH.; AUT; DA. 1980; VOL. 36; NO 1-2; PP. 63-70; ABS. GER; BIBL. 27 REF.Article

HAMILTON'S LAW AND THE STABILITY OF NONCONSERVATIVE, CONTINUOUS SYSTEMSBAILEY CD.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 37-43; BIBL. 16 REF.Conference Paper

ACOUSTIC EMISSION FOR IN-FLIGHT MONITORING ON AIRCRAFT STRUCTURES. = EMISSION ACOUSTIQUE POUR LE CONTROLE EN VOL DES STRUCTURES D'AVIONSBAILEY CD.1976; MATER. EVALUAT.; U.S.A.; DA. 1976; VOL. 34; NO 8; PP. 165-171; BIBL. 10 REF.Article

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

THE METHOD OF RITZ APPLIED TO THE EQUATION OF HAMILTON. = LA METHODE DE RITZ APPLIQUEE A L'EQUATION D'HAMILTONBAILEY CD.1976; COMPUTER METHODS APPL. MECH. ENGNG; NETHERL.; DA. 1976; VOL. 7; NO 2; PP. 235-247; BIBL. 12 REF.Article

HAMILTON'S PRINCIPLE AND THE CALCULUS OF VARIATIONSBAILEY CD.1982; ACTA MECH.; ISSN 0001-5970; AUT; DA. 1982; VOL. 44; NO 1-2; PP. 49-57; BIBL. 19 REF.Article

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

HAMILTON'S LAW OR HAMILTON'S PRINCIPLE: A RESPONSE TO ULVI YURTSEVERBAILEY CD.1983; FOUNDATIONS OF PHYSICS; ISSN 0015-9018; USA; DA. 1983; VOL. 13; NO 5; PP. 539-544; BIBL. 28 REF.Article

VIBRATION AND LOCAL INSTABILITY OF THERMALLY STRESSED PLATESBAILEY CD.1981; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1981; VOL. 25; NO 3; PP. 263-278; BIBL. 26 REF.Article

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

VIBRATION OF THERMALLY STRESSED PLATES WITH VARIOUS BOUNDARY CONDITIONSBAILEY CD.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 1; PP. 14-19; BIBL. 10 REF.Serial Issue

ON A MORE PRECISE STATEMENT OF HAMILTON'S PRINCIPLEBAILEY CD.1981; FOUND. PHYS.; ISSN 0015-9018; USA; DA. 1981; VOL. 11; NO 3-4; PP. 279-296; BIBL. 29 REF.Article

HAMILTON'S LAW AND THE STABILITY OF NONCONSERVATIVE CONTINUOUS SYSTEMSBAILEY CD.1980; A.I.A.A. J., NEW YORK; USA; DA. 1980; VOL. 18; NO 3; PP. 347-349; BIBL. 11 REF.Article

EXACT AND DIRECT ANALYTICAL SOLUTIONS TO VIBRATING SYSTEMS WITH DISCONTINUITIES. = SOLUTIONS ANALYTIQUES EXACTES ET DIRECTES DES SYSTEMES VIBRANTS AVEC DISCONTINUITESBAILEY CD.1976; J. SOUND VIBR.; G.B.; DA. 1976; VOL. 44; NO 1; PP. 15-25; BIBL. 7 REF.Article

HAMILTON, RITZ, AND ELASTODYNAMICS.BAILEY CD.1976; J. APPL. MECH.; U.S.A.; DA. 1976; VOL. 43; NO 4; PP. 684-688; BIBL. 21 REF.Article

A NEW LOOK AT HAMILTON'S PRINCIPLE.BAILEY CD.1975; FOUND. OF PHYS.; U.S.A.; DA. 1975; VOL. 5; NO 3; PP. 433-451; BIBL. 7 REF.Article

ACOUSTIC EMISSION STRUCTURE-BORNE BACKGROUND NOISE MEASUREMENTS ON AIRCRAFT DURING FLIGHT. = MESURE DU BRUIT DE FOND PROVENANT DE LA STRUCTURE POUR L'EMISSION ACOUSTIQUE DANS UN AVION PENDANT LE VOLBAILEY CD; PLESS WM.1976; MATER. EVALUAT.; U.S.A.; DA. 1976; VOL. 34; NO 9; PP. 189-201 (8P.); BIBL. 2 REF.Article

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

VIBRATION AND STABILITY OF NON-CONVERVATIVE FOLLOWER FORCE SYSTEMSBAILEY CD; HAINES JL.1981; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1981; VOL. 26; NO 1; PP. 1-31; BIBL. 23 REF.Article