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BREVET 2.344.720 (A2) (77 07929). - 17 MARS 1977. PERFECTIONNEMENT AUX TUYERES DE TURBOMACHINES.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

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

BREVET 2.333.966 (A1) (76 26389). - 1ER SEPTEMBRE 1976. TUYERE DE PROPULSION A SECTION VARIABLE.sdPatent

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

Optical and thermal characterization procedure for a variable geometry concentrator: A standard approachSALLABERRY, Fabienne; PUJOL-NADAL, Ramón; MARTINEZ-MOLL, Victor et al.Renewable energy. 2014, Vol 68, pp 842-852, issn 0960-1481, 11 p.Article

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

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

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

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

VARIABLE CYCLE ENGINES. THE NEXT STEP IN PROPULSION EVOLUTION.JOHNSON JE.1976; IN : PROPUL. CONF. 12; PALO ALTO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 758; PP. 1-38Conference Paper

Special Issue on Moprhing Aircraft - Part IIFRISWELL, Michael I; WERELEY, Norman M.Journal of intelligent material systems and structures. 2011, Vol 22, Num 10, issn 1045-389X, 149 p.Serial Issue

Special Issue on Morphing Aircraft- Part IFRISWELL, Michael I; WERELEY, Norman.Journal of intelligent material systems and structures. 2011, Vol 22, Num 9, issn 1045-389X, 154 p.Serial Issue

Analysis of Transition Stability for Morphing AircraftSEIGLER, T. M; NEAL, D. A.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 6, pp 1947-1954, issn 0731-5090, 8 p.Article

ECCENTRIC CAM DRIVE VARIES VALVE TIMINGSCOTT D ED; YAMAGUCHI J ED.1980; AUTOMAT. ENG.; ISSN 0098-2571; USA; DA. 1980; VOL. 88; NO 10; PP. 120-124Article

TESTS OF AN IMPROVED ROTATING STALL CONTROL SYSTEM ON A J-85 TURBOJET ENGINELUDWIG GR; NENNI JP.1980; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1980; VOL. 102; NO 4; PP. 903-911; BIBL. 4 REF.Article

VARIABLE AREA TURBOCHARGER FOR HIGH OUTPUT DIESEL ENGINESBERENYI SG; RAFFA CJ.1979; SAE TRANS.; ISSN 0096-736X; USA; DA. 1979 PUBL. 1980; VOL. 88; SECT. 1; PP. 271-286; BIBL. 5 REF.Article

AEROTHERMODYNAMIC PERFORMANCE OF A VARIABLE NOZZLE POWER TURBINE STAGE FOR AN AUTOMOTIVE GAS TURBINE.RAZINSKY EH; KUZIAK WR JR.1977; J. ENGNG POWER; U.S.A.; DA. 1977; VOL. 99; NO 4; PP. 587-592; BIBL. 8 REF.Article

AN ANALYTICAL STUDY OF THE EFFECTS OF TURBINE VARIABLE GEOMETRY OPERATION ON TURBINE BLADE COOLING REQUIREMENTS FOR FIXED MATCH POINT TURBOJET APPLICATION.NEALY DA; LUEDERS HG.1976; S.A.E. TRANS.; U.S.A.; DA. 1976 PARU 1977; VOL. 85; PART. 4; PP. 2864-2879; BIBL. 2 REF.Article

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