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PROSPECTS FOR VARIABLE GEOMETRY COMPRESSORS IN AUTOMOTIVE GAS TURBINES. = RECHERCHE SUR DES COMPRESSEURS A GEOMETRIE VARIABLE POUR TURBINES A GAZ DE VEHICULESHULHAN GM.1974; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1974; NO 2; PP. 15-24; BIBL. 4 REF.Article
ZUR THEORIE DER VERAENDERLICHEN TRAGFLUEGELPFEILUNG. = THEORIE DE L'AILE A GEOMETRIE VARIABLEKORDIK EJT.1974; OESTERR. INGR-Z.; OESTERR.; DA. 1974; VOL. 17; NO 12; PP. 418-427; BIBL. 14 REF.Article
BREVET 2.291.382 (A1) (7440663). - 18 NOVEMBRE 1974. TURBINES EOLIENNES ET DIVERS DISPOSITIFS POUR LEURS INSTALLATIONS, Y COMPRIS RESERVOIRS D'ENERGIES ET REGULATEURS AUTOMATIQUES DE TYPES NOUVEAUX.sdPatent
NEW ENGINE CYCLES. OPPORTUNITY FOR CREATIVITYSWAN WC; SCHOTT GJ.1975; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1975; VOL. 13; NO 1; PP. 24-35; BIBL. 2 REF.Article
2.289.747 (A1) (7533350). -31OCTOBRE 1975. TUYERE DE POUSSEE AVEC CHEMISE DE REFROIDISSEMENTsdPatent
SEPARATION EXPERIMENTALE DES INTENSITES DU COURANT CONVECTIF ET DU COURANT DE DEPLACEMENT DANS LES DIODES A GEOMETRIE ET TEMPERATURE DE LA CATHODE VARIABLESDYMSHITS YU I.1975; ZH. TEKH. FIZ.; S.S.S.R.; DA. 1975; VOL. 45; NO 8; PP. 1730-1734; BIBL. 5 REF.Article
BREVET 2.344.720 (A2) (77 07929). - 17 MARS 1977. PERFECTIONNEMENT AUX TUYERES DE TURBOMACHINES.sdPatent
VARIABLE-CYCLE ENGINES FOR SUPERSONIC CROISING AIRCRAFT.WILLIS EA; WELLIVER AD.1976; IN: PROPUL. CONF. 12; PALO ALTO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 759; PP. 1-11; BIBL. 22 REF.Conference Paper
VARIABLE COMPRESSOR GEOMETRY IN THE SINGLE-SHAFT AUTOMOTIVE TURBINE ENGINE = COMPRESSEUR A GEOMETRIE VARIABLE POUR UN MOTEUR A TURBINE D'AUTOMOBILE A UN SEUL ARBRESHERIDAN DC; NORDENSON GE; AMANN CA et al.1974; S.A.E. TRANS.; U.S.A.; DA. 1974; VOL. 83; NO PART. 1; PP. 753-764; BIBL. 16REF.Article
BREVET 2.333.966 (A1) (76 26389). - 1ER SEPTEMBRE 1976. TUYERE DE PROPULSION A SECTION VARIABLE.sdPatent
ECHO WAVEFORM SYNTHESIS IN A RAPIDLY VARYING GEOMETRYRICKER DW.1982; JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA; ISSN 0001-4966; USA; DA. 1982; VOL. 72; NO 4; PP. 1321-1323; BIBL. 4 REF.Article
AERODYNAMIC DESIGN OF FIXED AND VARIABLE GEOMETRY NOZZLE LESS TURBINE CASINGSCHAPPLE PM; FLYNN PF; MULLOY JM et al.1980; J. ENGNG POWER; USA; DA. 1980; VOL. 102; NO 1; PP. 141-147; BIBL. 12 REF.Article
PROSPECTS FOR VARIABLE GEOMETRY COMPRESSOS IN AUTOMOTIVE GAS TURBINES = RECHERCHE SUR DES COMPRESSEURS A GEOMETRIE VARIABLE POUR TURBINES A GAZ DE VEHICULESHUL HAN GM.1974; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1974; NO 2; PP. 15-24; BIBL. 4 REF.Article
VARIABLE AREA RADIAL-INFLOW TURBINEFLAXINGTON D; SZCZUPAK DT.1982; TURBOCHARGING AND TURBOCHARGERS. CONFERENCE/1982-04-26/LONDON; GBR; LONDON: THE INSTITUTION OF MECHANICAL ENGINEERS; DA. 1982; PP. 55-62; BIBL. 7 REF.Conference Paper
UNE NOUVELLE CHAMBRE DE COMBUSTION POUR MOTEUR DIESEL: LA CHAMBRE A GEOMETRIE VARIABLEBRISSON R; ECOMARD A; EYZAT P et al.1972; ENTROPIE; FR.; DA. 1972; VOL. 8; NO 48; PP. 13-25; ABS. ANGL. ALLEM. ESP.; BIBL. 4 REF.Serial Issue
INFLUENCE COEFFICIENTS OF VARIABLE GEOMETRY FREE GAS TURBINE ENGINESHIRSCH M; ADLER D; DAYAN J et al.1982; ISRAEL JOURNAL OF TECHNOLOGY; ISSN 0021-2202; ISR; DA. 1982; VOL. 20; NO 1-2; PP. 37-47; BIBL. 3 REF.Article
UTILISATION DU GUEULARD A GEOMETRIE VARIABLE A NEUVES-MAISONS.HERBIN JL.1977; CENTRE DOCUMENT. SIDER., CIRC. INFORM. TECH.; FR.; DA. 1977; VOL. 34; NO 2; PP. 281-299; BIBL. 5 REF.Article
AEROTHERMODYNAMIC FACTORS GOVERNING THE RESPONSE RATE OF GAS TURBINESMACISAAC BD; SARAVANAMUTTOO HIH.1974; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1974; NO 3; PP. 23-35; BIBL. 9 REF.Article
TECHNOLOGY TRANSFER IN THE DESIGN OF ADJUSTABLE LINKAGESTAO DC; YAN HS.sdDESIGN ENGINEERING TECHNICAL CONFERENCE/1978/MINNEAPOLIS MN; USA; NEW YORK: AMERICAN SOCIETY OF MECHANICAL ENGINEERS; DA. S.D.; VOL. 67; PP. 1-4; BIBL. 2 REF.Conference Paper
BREVET 2.304.800 (A1) (76 06921). - 11 MARS 1976. DISPOSITIF D'ACTIONNEMENT A RETROACTION.sdPatent
VARIABLE GEOMETRY FOR SUPERSONIC MIXED-COMPRESSION INLETS.SORENSEN NE; LATHAM EA; SMELTZER DB et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 4; PP. 309-312; BIBL. 8 REF.Article
ZUM BETRIEBSVERHALTEN VON VERBUND-ZWEISTROM-TURBOLUFTSTRAHTRIEBWERKEN MIT VERSTELLBAREN DUESEN UND TURBINEN. = COMPORTEMENT OPERATIONNEL DES TURBOREACTEURS DOUBLE-FLUX AVEC TUYERES ET TURBINES VARIABLESRICK H; KURZKE J.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 5; PP. 268-275; ABS. ANGL. FR.; BIBL. 14 REF.Article
ON THE OPERATING CHARACTERISTICS OF THE VARIABLE GEOMETRY WIND TURBINETEODORESCU TINTEA C; DUMITRESCU H; SAVULESCU SN et al.1982; REV. ROUM. SCI. TECH., SER. MEC. APPL.; ISSN 0035-4074; ROM; DA. 1982; VOL. 27; NO 3; PP. 347-360; BIBL. 3 REF.Article
BREVET TURBINE A VOLET ARTICULE1978; ; FRA; DA. 1978-01-05; FR/A1/2.389.760; DEP.78-12932/1978-05-02; PR. EU/793.542/1977-05-04Patent
THE VARIABLE GEOMETRY VERTICAL AXIS WINDMILL.MUSGROVE PJ.1976; ENERGY DIGEST; G.B.; DA. 1976; VOL. 5; NO 6; PP. 10-11Article