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CALCUL DES CARACTERISTIQUES EXPERIMENTALES DES ETAGES DES TURBINES D'APRES LES RESULTATS DE LA TRAVERSEEKIRILLOV AI; AFANAS'EVA NN; AGAFONOV BN et al.1978; ENERGO-MASHINOSTR.; S.S.S.R.; DA. 1978; NO 4; PP. 43-45Article

STRUCTURE DU FLUX DERRIERE DES GRILLES ANNULAIRES AVEC UNE INCLINAISON TANGENTIELLE DE L'AILETTAGE DISTRIBUTEURMITYUSHKIN YU I; YAKOVLEV VP.1977; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1977; NO 11; PP. 67-72; BIBL. 7 REF.Article

HYPERSONIC FLOWFIELD MEASUREMENTS USING LASER-RAMAN SPECTROSCOPY. = MESURE DES CHAMPS D'ECOULEMENT HYPERSONIQUES A L'AIDE DE LA SPECTROSCOPIE RAMAN A LASERWILLIAMS WD; LEWIS JWL.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1269-1270; BIBL. 7 REF.Article

INTEGRATED SCRAMJET NOZZLE/AFTERBODY PERFORMANCE ANALYSIS.SADUNAS JA.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1297; PP. 1-9; BIBL. 12 REF.Conference Paper

TRANSONIC AIRFOIL ANALYSIS AND DESIGN USING CARTESIAN COORDINATES. = ANALYSE ET CONCEPTION DES PROFILS AERODYNAMIQUES TRANSSONIQUES A L'AIDE DES COORDONNEES CARTESIENNESCARLSON LA.1975; IN: COMPUT. FLUID DYN. CONF. 2. PROC.; HARTFORD, CONN.; 1975; S.L.; AIAA; DA. 1975; PP. 175-183; BIBL. 18 REF.Conference Paper

CALCUL DU CHAMP D'ECOULEMENT D'UN ETAGE DE COMPRESSEURCAMEK J.1975; STROJN. CAS.; CESKOSL.; DA. 1975; VOL. 26; NO 3; PP. 251-264; ABS. RUSSE ANGLArticle

PERFORMANCE OF ROTATING CASCADES UNDER THE INLET-DISTORTIONS. II: PERFORMANCE UNDER THE CIRCUMFERENTIAL DISTORTIONSSEO N; NAKATANI T; TANAKA S et al.1981; BULL. JSME; ISSN 0021-3764; JPN; DA. 1981; VOL. 24; NO 190; PP. 628-633; BIBL. 14 REF.Article

FLOW IN TRANSONIC COMPRESSORSKERREBROCK JL.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 1; PP. 4-19; BIBL. 50 REF.Article

BERECHNUNG DER STROMFLAECHEN IN EINER HYDRODYNAMISCHEN MASCHINE = CALCUL DES SURFACES D'ECOULEMENT DANS UNE MACHINE HYDRODYNAMIQUEFLEISCHNER P.1981; PUBL. TECH. UNIV. HEAVY IND., SER. C; ISSN 0133-297X; HUN; DA. 1981; VOL. 35; NO 1; PP. 33-52; ABS. ENG/RUSArticle

CALCULATION OF TRANSONIC FLOW AROUND AXISYMMETRIC INLETS.ARLINGER BG.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1614-1621; BIBL. 12 REF.Article

STRUCTURE D'UN ECOULEMENT DERRIERE DES GRILLES DIRECTRICES ANNULAIRES A DEUX RANGSMITYUSHKIN YU I; OSINKIN VN.1979; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; BYS; DA. 1979; VOL. 22; NO 6; PP. 39-43; BIBL. 6 REF.Article

ON A CONSISTENT MODEL OF BLADE-TO-BLADE FLOW THROUGH AN AXIAL TURBOMACHINEFRITH DA.sdAUSTRALASIAN CONFERENCE ON HYDRAULICS AND FLUID. 7/1980/BRISBANE; AUS; BARTON: INSTITUTION OF ENGINEERS, AUSTRALIA; DA. S.D.; PP. 389-392; BIBL. 7 REF.Conference Paper

FLOWFIELD IN THE PLANE OF SYMMETRY BELOW A DELTA WING.CRAMER MS; GEORGE AR; SEEBASS AR et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 2; PP. 212-215; BIBL. 2 REF.Article

ULTRASONIC METHOD FOR FLOW FIELD MEASUREMENT IN WIND TUNNEL TESTSENGLER RH; SCHMIDT DW; WAGNER WJ et al.1982; J. ACOUST. SOC. AM.; ISSN 0001-4966; USA; DA. 1982; VOL. 71; NO 1; PP. 41-50; BIBL. 14 REF.Article

ECOULEMENT AUTOUR D'UN PROFIL DISPOSE SOUS UN ANGLE D'ATTAQUE DANS UN ECOULEMENT SONIQUE INCIDENTLICHUK ST; FAL'KOVICH SV.1982; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 5; PP. 81-86; BIBL. 4 REF.Article

SURVEY OF METHODS FOR EXHAUST-NOZZLE FLOW ANALYSIS.BROWN EF; HAMILTON GL.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 4-11; BIBL. 1 P. 1/2Article

INFLUENCE DU CHAMP D'ECOULEMENT SUR LE RAYON MOYEN D'UN ETAGE DE COMPRESSEURVORACEK V.1976; STROJN. CAS.; CESKOSL.; DA. 1976; VOL. 27; NO 3; PP. 241-256; BIBL. 1 REF.Article

EXPERIMENTAL EVALUATION OF AN ANALYTICALLY DERIVED BLEED SYSTEM FOR A SUPERSONIC INLET.SYBERG J; KONCSEK JL.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1210; PP. 1-6; BIBL. 5 REF.Conference Paper

DIE WAERMEUEBERTRAGUNG BEIM SIEDEN UNTER DEM EINFLUSS HYDRODYNAMISCHER VORGAENGE. = INFLUENCE DES PROCESSUS HYDRODYNAMIQUES SUR LE TRANSFERT DE CHALEUR A L'EBULLITIONBEST R; BUROW P; BEER H et al.1975; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1975; VOL. 18; NO 9; PP. 1037-1047; ABS. ANGL. FR. RUSSE; BIBL. 19 REF.Article

MESURE ET ANALYSE DU CHAMP D'ECOULEMENT AUTOUR D'UNE MAQUETTE HYDRODYNAMIQUE INWID AVEC REFERENCE PARTICULIERE A L'EFFET D'ABRIKITAZAWA T; INUI T; KAJITANI H et al.1974; J. SOC. NAV. ARCHITECTS JAP.; JAP.; DA. 1974; VOL. 135; PP. 1-11; ABS. ANGL.; BIBL. 7 REF.Article

HYDRAULIC EXPONENTSVEN TE CHOW.1981; PROC. AM. SOC. CIV. ENG., J. HYDRAUL. DIV.; ISSN 0044-796X; USA; DA. 1981; VOL. 107; NO 11; PP. 1489-1499; BIBL. 11 REF.Article

STREAMWISE DEVELOPMENT OF THE FLOW OVER A DELTA WINGSFORZA PM; SMORTO MJ.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 7; PP. 833-834; BIBL. 7 REF.Article

A DIRECT-INVERSE TECHNIQUE FOR LOW SPEED HIGH LIFT AIRFOIL FLOWFIELD ANALYSISCARLSON LA.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 26.1-26.10; BIBL. 18 REF.Article

AN EXPERIMENTAL STUDY OF THREE-DIMENSIONAL CHARACTERISTICS OF PROPELLER WAKES UNDER STALLING CONDITIONS.FAVIER D; REBONT J; MARESCA C et al.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 4; PP. 745-752; BIBL. 18 REF.Article

LAMINAR SEPARATION ON A BLUNTED CONE AT HIGH ANGLES OF ATTACK. = DECOLLEMENT LAMINAIRE SUR UN CONE EMOUSSE AUX INCIDENCES ELEVEESLUBARD SC.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 32.1-32.11; BIBL. 27 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

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