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LA SOUFFLANTE A PAS VARIABLE: ASPECTS TECHNIQUESDAVIS DGM.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 885-886Serial Issue

INSTALLATION CAUSED FLOW DISTORTION AND ITS EFFECT ON NOISE FROM A FAN DESIGNED FOR TURBOFAN ENGINES = DISTORTION DE L'ECOULEMENT DU A L'INSTALLATION ET SON EFFET SUR LE BRUIT D'UNE SOUFFLANTE CONCUE POUR TURBOREACTEUR A SOUFFLANTE CANALISEEPOVINELLI FP; DITTMAR JH.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-10; BIBL. 12 REF.Conference Paper

REDUCTION OF JT8D POWERED AIRCRAFT NOISE BY ENGINE REFANNING = REDUCTION DU BRUIT DES AVIONS A MOTEUR JT8D PAR MODIFICATION DE LA TURBO-SOUFFLANTESTITT LE; MEDEIROS AA.1974; S.A.E. TRANS.; U.S.A.; DA. 1974; VOL. 83; NO PART. 2; PP. 1859-1870; BIBL. 8 REF.Article

PROP-FAN. A HIGH THRUST, LOW NOISE PROPULSORROSEN G.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1654-1664; BIBL. 12 REF.Serial Issue

TURBOFAN TRENDS FOR SHORT HAUL = ORIENTATIONS DU TURBOREACTEUR A SOUFFLANTE CANALISEE POUR COURT COURRIERDAWSON LG; SILLS TD.1971; IN: GAS TURBINE FLUIDS ENG. CONF. PROD. SHOW. SAN FRANCISCO, CALIF., 1972; HEADQUARTERS; A.S.M.E.; DA. 1971; VOL. 86; PP. 1-12Conference Paper

LOW PRESSURE RATIO FAN NOISE EXPERIMENT AND THEORYMETZGER FB; HANSON DB.1973; J. ENGNG POWER; U.S.A.; DA. 1973; VOL. 95; NO 1; PP. 19-26; BIBL. 13 REF.Serial Issue

MODERN ELECTRICAL EQUIPMENT FOR BLAST FURNACE BLOWERNISHIJIMA K; TAKITA M.1975; TOSHIBA REV., INTERNATION. ED.; JAP.; DA. 1975; NO 97; PP. 13-18Article

NEW TURBOFAN ENGINES: F101 AND TF34 = NOUVEAUX TURBOREACTEURS SOUFFLANTE CANALISEE: F101 ET TF34WORSHAM JE.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 841; PP. 1-5Conference Paper

ESSAI D'EXPLOITATION DES CONDUITS D'AIR DE SOUFFLAGE FROID DANS LE SCHEMA DE LIAISON DIRECTE SOUFFLERIE-HAUT FOURNEAUKHUDYK IN.1975; PROMYSHL. ENERGET.; S.S.S.R.; DA. 1975; NO 10; PP. 22-23; BIBL. 2 REF.Article

LE ROLLS-ROYCE RB. 211. UN PROGRAMME COUTEUX MAIS PROMETTEURNIBLOE M.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 856-858Serial Issue

SOME ASPECTS OF FAN NOISE SUPPRESSION USING HIGH MACH NUMBER INLETS.SAVKAR SD; KAZIN SB.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 554; PP. 1-13; BIBL. 10 REF.Conference Paper

NEUE ERKENNTNISSE UEBER BRENNERGEBLAESE = NEW KNOWLEDGES OF BURNER FANS = RESULTATS NOUVELLEMENT OBTENUS EN CE QUI CONCERNE LES SOUFFLANTES DE BRULEURSFRITSCH WH.1982; GAS WAERME INT.; ISSN 0020-9384; DEU; DA. 1982; NO 2-3; PP. 93-100; BIBL. 7 REF.Article

REGULATION AUTOMATIQUE DES SOUFFLANTES D'UN HAUT FOURNEAU A MARCHE EN PARALLELESARANTSEV KB; SERGEEV BM; MINUKHIN EM et al.1976; STAL; S.S.S.R.; DA. 1976; NO 5; PP. 400Article

BREVET 2.301.708 (A1) (75 05196). - 19 FEVRIER 1975. SOUFFLANTE RADIALE.sdPatent

DESIGN COMPARISON OF QUIET M=0.80 STOL TRANSPORTSSCHERRER R; OLSON R.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2528-2537; BIBL. 27 REF.Serial Issue

2.262.201 (A1) (7505842). - 25FEVRIER 1975. CAPOTAGE POUR SOUFFLANTE DE TURBOMOTEUR.sdPatent

2.262.200 (A1) (7505841). - 25FEVRIER 1975. TURBO-MOTEUR A SOUFFLANTE A TAUX DE DILUTION VARIABLE.sdPatent

2.270.450 (A1) (7411300). - 29 MARS 1974. INSTALLATION MOTRICE A TURBINE A GAZ A DEUX OU PLUSIEURS FLUXsdPatent

2.272.279 (A1) (75 16081). - 23 MAI 1975. METHODE DE FABRICATION D'UNE ROUE DE SOUFFLANTE, ET ROUE OBTENUEsdPatent

SOME AERODYNAMIC DESIGN CONSIDERATIONS FOR HIGH BYPASS RATIO FANS.SMITH LH JR.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (14P.); BIBL. 5 REF.Conference Paper

DAS QUERSTROMGEBLAESE IM INDUSTRIEOFENBAU. = THE CROSS-FLOW BLOWER IN INDUSTRIAL FURNACES = LA SOUFFLANTE A COURANT TRANSVERSAL DANS LES FOURS INDUSTRIELSGILLHAUS H.1976; GAS WAERME INTERNATION.; DTSCH.; DA. 1976; VOL. 25; NO 1-2; PP. 46-49; ABS. ANGL. FR.; BIBL. 5 REF.; (KOLLOQ. INDUSTRIEOFENBAU. 2. VORTR.; AACHEN; 1976)Conference Paper

REGENERATIVE TURBOFANS: A COMPARISON WITH NONREGENERATIVE UNITSKENTFIELD JAC.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 174-181; BIBL. 9 REF.Article

NATURAL CONVECTION IN AIRCRAFT FUEL TANKS = CONVECTION NATURELLE DANS LES RESERVOIRS DE COMBUSTIBLE DES AVIONSMALLINSON GD; DE VAHL DAVIS G.1973; ISRAEL J. TECHNOL.; ISRAEL; DA. 1973; VOL. 11; NO 1-2; PP. 89-101; BIBL. 28 REF.; (PROC. 15TH ISR. ANNU. CONF. AVIAT. ASTRONAUT.; TEL AVIV; 1973)Conference Paper

UNE FORCE AERIENNE NEUTRE ENTRE LES BLOCS: L'HISTOIRE DU VIGGENREGELIN K; CHOPPING D.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 3; PP. 221-228Serial Issue

NASA LIFT FAN V/STOL TRANSPORT TECHNOLOGY STATUS = ETAT DE LA TECHNOLOGIE DU TRANSPORT ADAC/V A SOUFFLANTE DE SUSTENTATION A LA NASADECKERT WH; EVANS RC.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 856; PP. 1-7; H.T. 5; BIBL. 6 REF.Conference Paper

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