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Results 1 to 25 of 875

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INTERACTION AERODYNAMIQUE DES GRILLES MOBILES A PROFILSGNESIN VI.1982; IZV. AKAD. NAUK SSSR, ENERG. TRANSP.; ISSN 0002-3310; SUN; DA. 1982; NO 1; PP. 102-109; BIBL. 10 REF.Article

SUPERSONIC CASCADE FLOW.LICHTFUSS HJ; STARKEN H.1974; PROGR. AEROSPACE SCI.; G.B.; DA. 1974; VOL. 15; PP. 37-149; ABS. ALLEM. FR.; BIBL. 4 P. 1/2Article

A THEORETICAL MODEL FOR PREDICTING THE PERFORMANCE OF CIRCULATION CONTROLLED AEROFOILS AND CASCADESFLINT WL; HOLLIDAY CI.1982; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1982; VOL. 86; NO 852; PP. 76-82; BIBL. 13 REF.Article

EINFACHES UMBEWERTUNGSVERFAHREN FUER DIE GESCHWINDIGKEITSVERTEILUNG AUF BELIEBIGEN GITTERPROFILEN KLEINEN TEILUNGSVERHAELTNISSES = METHODE SIMPLE D'EVALUATION POUR LA DISTRIBUTION DE VITESSE SUR DES CASCADES DE PROFILS QUELCONQUES AVEC FAIBLE ESPACEMENTHACKESCHMIDT M.1981; MASHINENBAUTECHNIK; ISSN 0025-4495; DDR; DA. 1981; VOL. 30; NO 6; PP. 279-281; ABS. ENG/RUS; BIBL. 5 REF.Article

SECONDARY FLOW IN CASCADES: THE EFFECT OF AXIAL VELOCITY RATIO.MARSH H.1974; J. MECH. ENGNG SCI.; G.B.; DA. 1974; VOL. 16; NO 6; PP. 402-407; BIBL. 5 REF.Article

THE EFFECTS OF TRAILING VORTICITY ON THE FLOW THROUGH HIGHLY LOADED CASCADES.MCCUNE JE; HAWTHORNE WR.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 74; NO 4; PP. 721-740; BIBL. 20 REF.Article

APPLICATION DU PROCESSUS DE STABILISATION PAR RAPPORT AU TEMPS POUR LA RESOLUTION DES PROBLEMES D'ECOULEMENT STATIONNAIRE AUTOUR DE GRILLES DE PROFILSBOGOD AB; ZAMTFORT BS; IVANOV M YA et al.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 118-124; BIBL. 13 REF.Article

COMPUTATIONS OF UNSTEADY TRANSONIC CASCADE FLOWSNIXON D.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 790-792; BIBL. 3 REF.Article

A NEW APPROACH IN CASCADE FLOW ANALYSIS USING THE FINITE ELEMENT METHODBASKHARONE E; HAMED A.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 1; PP. 65-71; BIBL. 18 REF.Article

LIFTING AND NONLIFTING KERNEL FUNCTIONS FOR CASCADE AND ISOLATED AIRFOILSCHI MR.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 10; PP. 1265-1268; BIBL. 7 REF.Article

A FINITE ELEMENT ANALYSIS OF UNSTEADY DIAGONAL CASCADE FLOWSDAIGUJI H; SHIRAHATA H.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 180; PP. 888-894; BIBL. 11 REF.Article

AEROELASTIC STABILITY ANALYSIS OF SUPERSONIC CASCADESSTRADA JA; CHADWICK WR; PLATZER MF et al.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 4; PP. 533-541; BIBL. 28 REF.Article

CONFORMAL REPRESENTATION OF ARBITRARY MULTICONNECTED AIRFOIL SECTIONS.PROSNAK WJ.1977; BULL. ACAD. POLON. SCI., SCI. TECH.; POLOGNE; DA. 1977; VOL. 25; NO 7; PP. 25-36; ABS. RUSSE; BIBL. 11 REF.Article

SHORT INFORMAL ADDITIONAL PRESENTATIONS.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 214; PP. (45P.); BIBL. DISSEM.; (SECONDARY FLOWS TURBOMACH. AGARD PROPUL. ENERG. PANEL. 49. PROC.; THE HAGUE, NETH.; 1977)Conference Paper

UNSTEADY WAKE MEASUREMENTS OF AIRFOILS AND CASCADES.SATYANARAYANA B.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 5; PP. 613-618; BIBL. 15 REF.Article

PERTES DE PROFIL LORS DE L'ECOULEMENT NON STATIONNAIRE AUTOUR DES RESEAUX ACTIFS DE TRAVAILSAMOJLOVICH GS; YABLOKOV LD; RABOTAEV VG et al.1977; TEPLOENERGETIKA; S.S.S.R.; DA. 1977; NO 2; PP. 40-42; BIBL. 7 REF.Article

NUMERICAL COMPUTATION OF NONSTATIONARY AERODYNAMICS OF FLAT PLATE CASCADES IN COMPRESSIBLE FLOW.NI RH; SISTO F.1975; IN: GAS TURBINE CONF. PROD. SHOW; HOUSTON, TEX.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 75-GT5; PP. 1-6; BIBL. 17 REF.Conference Paper

UNSTEADY SUPERSONIC CASCADE IN SUBSONIC AXIAL FLOW.VERDON JM; MCCUNE JE.1975; A.I.A.A., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 2; PP. 193-201; BIBL. 19 REF.Article

RESEARCHES ON THE TWO-DIMENSIONAL CASCADE. V. ON THE PERFORMANCE OF FLATPLATE CASCADE.IKUI T; INOUE M; KANEKO K et al.1974; BULL. J.S.M.E.; JAP.; DA. 1974; VOL. 17; NO 112; PP. 1260-1266; BIBL. 9 REF.Article

FINITE ELEMENT ANALYSIS OF TRANSONIC FLOWS IN HIGHLY STAGGERED CASCADESAKAY HU; ECER A.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 9 P.; BIBL. 10 REF.Conference Paper

NUMERICAL TREATMENT OF UNSTEADY SUBSONIC FLOW PAST AN OSCILLATING CASCADECASPAR JR; VERDON JM.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 12; PP. 1531-1539; BIBL. 11 REF.Article

SULL'IMPIEGO DI UNA SEMPLICE TRASFORMAZIONE CONFORME PER LO STUDIO DI PROFILI "PSEUDO-JOUKOWSKI" IN SCHIERA = SUR L'EMPLOI D'UNE TRANSFORMATION CONFORME SIMPLE POUR L'ETUDE D'UN PROFIL "PSEUDO-JOUKOWSKI" EN CASCADEBENVENUTO G.1981; TERMOTECNICA; ISSN 0040-3725; ITA; DA. 1981; VOL. 35; NO 5; PP. 271-278; ABS. ENG; BIBL. 25 REF.Article

A COORDINATE SYSTEM FOR A VISCOUS TRANSONIC CASCADE ANALYSIS.EISEMAN PR.1978; J. COMPUT. PHYS.; U.S.A.; DA. 1978; VOL. 26; NO 3; PP. 307-338; BIBL. 1 P. 1/2Article

ROTOR DESIGN TO ATTENUATE FLOW DISTORTION. II. AN UNSTEADY THIN AIRFOIL CASCADE ANALYSIS.SAVELL CT; WELLS WR.1975; J. ENGNG POWER; U.S.A.; DA. 1975; VOL. 97; NO 1; PP. 37-46; BIBL. 16 REF.Article

ECOULEMENT TRIDIMENSIONNEL STATIONNAIRE D'UN FLUIDE PARFAIT SUR DES SYSTEMES DE PALES DE TURBOMACHINESMORGUNOV GM.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 6; PP. 3-12; BIBL. 7 REF.Article

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