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ANALYSE DE L'INFLUENCE DE LA TURBULENCE ATMOSPHERIQUE SUR LE NIVEAU DES CONTRAINTES VARIABLES DE FLEXION DANS LES PALES DE L'HELICE PORTEUSE D'UN HELICOPTERETURKINA AI.1980; IZV. VYSS. UCEBN. ZAVED., AVIAC. TEH.; ISSN 0579-2975; SUN; DA. 1980; NO 2; PP. 83-86; BIBL. 4 REF.Article

A LINEAR PROGRAMMING APPROACH FOR BALANCING FLEXIBLE ROTORS.LITTLE RM; PILKEY WD.1976; J. ENGNG INDUSTRY; U.S.A.; DA. 1976; VOL. 98; NO 3; PP. 1030-1035; BIBL. 6 REF.Article

STABILITE ET AUTO-OSCILLATIONS DES ROTORS COAXIAUXPOZNYAK EH L.1982; MEH. TVERD. TELA; ISSN 0572-3299; SUN; DA. 1982; NO 2; PP. 38-45; BIBL. 9 REF.Article

THEORETICAL AND EXPERIMENTAL DETERMINATION OF A AERODYNAMIC CHARACTERISTICS OF A HELICOPTER ROTORD'ANGELO S; MALVANO R.1979; MECCANICA; ITA; DA. 1979; VOL. 14; NO 1; PP. 26-33; ABS. ITA; BIBL. 7 REF.Article

DER EINFLUSS VON KREISELWIRKUNG, SCHUBNACHGIEBIGKEIT UND LAGERELASTIZITAET AUF DIE LAGE DER KRITISCHEN DREHZAHLEN EINFACHER ROTOREN. = INFLUENCE DE L'EFFET GYROSCOPIQUE, DE LA FLEXIBILITE DE CISAILLEMENT ET DE L'ELASTICITE DES PALIERS SUR LA POSITION DE LA VITESSE CRITIQUE DE ROTORS SIMPLESGASCH R; THORMANN J.1977; FORSCH. IM INGR-WES.; DTSCH.; DA. 1977; VOL. 43; NO 4; PP. 101-109; ABS. ANGL.; BIBL. 4 REF.Article

NOISE GENERATION BY TRANSONIC OPEN ROTORSHAWKINGS DL.1979; MECHANICS OF SOUND GENERATION IN FLOWS. SYMPOSIUM/1979/GOETTINGEN; DEU/USA; BERLIN: SPRINGER-VERLAG/HEIDELBERG: SPRINGER-VERLAG/NEW YORK: SPRINGER-VERLAG; DA. 1979; PP. 294-300; BIBL. 4 REF.Conference Paper

STEADY-STATE UNBALANCE RESPONSE OF A THREE-DISK FLEXIBLE ROTOR ON FLEXIBLE, DAMPED SUPPORTS.CUNNINGHAM RE.1978; J. MECH. DESIGN; USA; DA. 1978; VOL. 100; NO 3; PP. 563-573; BIBL. 15 REF.Article

DYNAMIQUE D'UNE MACHINE A ROTOR VERTICALKEL'ZON AS; BOGORAD EH E.1978; VEST. MASHINOSTR.; SUN; DA. 1978; VOL. 58; NO 8; PP. 16-20; BIBL. 5 REF.Article

VORTEX THEORY FOR HOVERING ROTORSMILLER RH.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1754-1756; BIBL. 16 REF.Article

STABILITY ANALYSIS OF MULTI-SPAN ROTOR SYSTEM AND ITS APPLICATION 3-THEORY OF MULTI-SPAN ROTOR AND ITS EXPERIMENTIWATSUBO T; OKAUE M; KAWAI R et al.1982; BULL. JSME; ISSN 0021-3764; JPN; DA. 1982; VOL. 25; NO 199; PP. 88-94; BIBL. 4 REF.Article

STABILITY PROBLEMS OF ROTOR SYSTEMSIWATSUBO T.1980; SHOCK VIB. DIG.; USA; DA. 1980; VOL. 12; NO 7; PP. 3-8; BIBL. 65 REF.Article

THEORIE TURBULENTE DE L'HELICE DE SUSTENTATIONANIKIN VA.1982; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 5; PP. 169-172; BIBL. 7 REF.Article

WIND TUNNEL EVALUATION OF AEROELASTICALLY CONFORMABLE ROTORSBLACKWELL RH; MURRILL RJ; YEAGER WT JR et al.1981; J. AM. HELICOPTER SOC.; ISSN 0002-8711; USA; DA. 1981; VOL. 26; NO 2; PP. 31-39; BIBL. 4 REF.Article

RESIDUAL-FLEXIBILITY CORRECTIONS FOR TRANSIENT MODAL ROTORDYNAMIC MODELS.CHILDS DW; BATES JB III.1978; J. MECH. DESIGN; USA; DA. 1978; VOL. 100; NO 2; PP. 251-256; BIBL. 10 REF.Article

REPARATURMOEGLICHKEITEN AN HEISSTEILEN VON GASTURBINEN. = POSSIBILITIES FOR GAS TURBINE HIGH TEMPERATURE COMPONENT REPAIR = POSSIBILITES DE REPARATION DE LA PARTIE HAUTE TEMPERATURE DES TURBINES A GAZVAN SCHAIK T.1978; V.G.B. KRAFTWERKSTECH.; DTSCH.; DA. 1978; VOL. 58; NO 5; PP. 330-336; ABS. ANGL. NEERL. ITAL. FR. DAN.Article

Q-FACTOR ANALYSIS OF UNBALANCE VIBRATION IN ROTOR-BEARING SYSTEMSMATSUSHITA O; IDA M; KIKUCHI K et al.1982; BULL. JSME; ISSN 0021-3764; JPN; DA. 1982; VOL. 25; NO 200; PP. 265-276; BIBL. 8 REF.Article

OSCILLATIONS FORCEES DES ROTORS FLEXIBLES SUR DES PALIERS ANISOTROPESLISITSYN IS.1980; ENERGO-MASHINOSTR.; SUN; DA. 1980; NO 2; PP. 8-10; BIBL. 2 REF.Article

EIN NEUES VERFAHREN ZUR BERECHNUNG VON ZWANGSSCHWINGUNGEN ELASTISCHER ROTOREN UND FOLGERUNGEN FUER DAS AUSWUCHTEN. GREEN'SCHE RESOLVENTE, ENDWUCHTUNG OHNE TESTLAUF, EIGENSCHAFTEN DES KRAEFTEFREIEN ROTORS, MASSE FUER WUCHTGUETE, ALLGEMEINE KRITERIEN FUER DIE WAHL DER "N"-BZW. "N+2"-METHODE = UN NOUVEAU PROCEDE DE CALCUL DES VIBRATIONS FORCEES DES ROTORS ELASTIQUES ET LES CONSEQUENCES POUR L'EQUILIBRAGE. RESOLVANTE DE GREEN, EQUILIBRAGE FINAL SANS ESSAI, PROPRIETES D'UN ROTOR NE SUBISSANT PAS D'EFFORTS EXTERIEURS, MESURE DE LA QUALITE DE L'EQUILIBRAGE, CRITERES GENERAUX POUR LE CHOIX DE LA METHODE N OU N+2KELKEL K.1978; V.D.I. BER.; DEU; DA. 1978; NO 320; PP. 61-68; BIBL. 7 REF.Article

BREVET PROCEDE D'USINAGE D'UN CORPS DE REVOLUTION PAR COUPE AU MOYEN D'UN OUTIL ROTATIF A ARETE TRANCHANTE CIRCULAIRE ET OUTIL ROTATIF POUR LA MISE EN OEUVRE DUDIT PROCEDE1978; ; FRA; DA. 1978-12-22; FR/A1/2.387.721; DEP.78 11340/1978-04-18; PR. SU/2.475.943/1977-04-19Patent

EFFECTS OF REYNOLDS NUMBER ON PERFORMANCE CHARACTERISTICS OF A CENTRIFUGAL COMPRESSOR, WITH SPECIAL REFERENCE TO CONFIGURATIONS OF IMPELLERS.MASHIMO T; WATANABE I; ARIGA I et al.1975; J. ENGNG POWER; U.S.A.; DA. 1975; VOL. 97; NO 3; PP. 361-368; BIBL. 19 REF.Article

BIEGESCHWINGUNGSVERHALTEN UNWUCHTIGER ELASTISCHER ROTOREN BEI DER RESONANZDURCHFAHRT = COMPORTEMENT VIBRATOIRE EN FLEXION D'UN ROTOR ELASTIQUE SANS BALOURD LORS DU PASSAGE PAR LA RESONANCEMARKERT R.1980; VDI - BER.; ISSN 0083-5560; DEU; DA. 1980; NO 381; PP. 155-160; BIBL. 8 REF.Conference Paper

ANALYSE DE LA REPONSE A UN SEISME D'UN ROTOR FLEXIBLE SUPPORTE PAR DES PALIERS A FILM FLUIDENAKAGAWA E; SUGITA T; AZUMA T et al.1978; ISHIKAWAJIMA-HARIMA ENGNG REV.; JAP.; DA. 1978; VOL. 18; NO 1; PP. 1-5; ABS. ANGL.Article

EINFLUSS DER FUNDAMENTPARAMETER AUF DEN UNWUCHTZUSTAND EINES ELASTISCH AUSGEWUCHTETEN ROTORS. = INFLUENCE DES PARAMETRES DE LA FONDATION SUR L'ETAT DE DESEQUILIBRE D'UN ROTOR EQUILIBRE ELASTIQUEMENTSTUHLER W; MOLLER D.1976; V.D.I. BER.; DTSCH.; DA. 1976; NO 269; PP. 151-158; BIBL. 6 REF.; (V.D.I.-SCHWINGUNGSTAG; HANNOVER; 1976)Conference Paper

NON LINEAR ROTOR DYNAMICS ANALYSISADAMS ML.1980; SHOCK VIB. DIG.; ISSN 0583-1024; USA; DA. 1980; VOL. 12; NO 11; PP. 13-16; BIBL. 16 REF.Article

SEISMIC RESPONSE OF A FLEXIBLE ROTORSHIMOGO T; AIDA Y; NAKANO M et al.1980; VIBRATIONS IN ROTATING MACHINERY. INTERNATIONAL CONFERENCE. 2/1980/CAMBRIDGE; GBR; LONDON: MECHANICAL ENGINEERING PUBLICATIONS; DA. 1980; PP. 321-326; BIBL. 4 REF.Conference Paper

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