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A REVIEW OF SEPARATION IN STEADY, THREE-DIMENSIONAL FLOW. = REVUE DU DECOLLEMENT EN ECOULEMENT TRIDIMENSIONNEL STATIONNAIRESMITH JHB.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 31.1-31.17; BIBL. 4 P.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

CALCUL DES CARACTERISTIQUES HYDRODYNAMIQUES TRANSITOIRES D'UNE GRILLE A PROFILS MINCES VENTILESEFREMOV II; SEMENENKO VN.1975; GIDROMEKHANIKA, U.S.S.R.; S.S.S.R.; DA. 1975; NO 31; PP. 3-14; BIBL. 10 REF.Article

ESSAI NUMERIQUE EN DYNAMIQUE DES GAZBELOTSERKOVSKIJ OM.1975; CHISLEMN. METODY MEKH. SPLOSHN. SREDY; S.S.S.R.; DA. 1975; VOL. 6; NO 4; PP. 10-20; BIBL. 1 P. 1/2Article

INFLUENCE DU CARACTERE DE LA REPARTITION DE LA CHARGE SUR L'ECOULEMENT DANS LA ROUE A AUBES D'UN COMPRESSEUR CENTRIFUGEBEKNEV VS; KUFTOV AF; MARTYNOV VM et al.1977; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; S.S.S.R.; DA. 1977; NO 4; PP. 96-99; BIBL. 6 REF.Article

AERODYNAMICS OF SLENDER ROLLING WINGS AT INCIDENCE IN SEPARATED FLOW.COHEN MJ; NIMRI D.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 886-893; BIBL. 12 REF.Article

EXPERIMENTAL STUDY OF SEPARATION FROM THE BASE OF A CONE AT SUPERSONIC SPEEDS.KAYSER LD; DANBERG JE.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1607-1609; BIBL. 8 REF.Article

SUBSONIC LOADS ON WINGS HAVING SHARP LEADING EDGES AND TIPS.KANDIL OA; MOOK DT; NAYFEH AH et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 62-63; BIBL. 10 REF.Article

SUPERSONIC FLOW PAST A SLENDER DELTA WING. AN EXPERIMENTAL INVESTIGATION COVERING THE INCIDENCE RANGE-5O <OU= ALPHA <OU= 50O.RICHARDS IC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 2; PP. 143-153; BIBL. 15 REF.Article

HIGH-LILFT AERODYNAMICS.SMITH AMO.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 6; PP. 501-530; BIBL. 1 P.Article

THE FLOW ABOUT THE TRAILING EDGE OF A SUPERSONIC OSCILLATING AEROFOIL. = ECOULEMENT AUTOUR DU BORD DE FUITE D'UN PROFIL AERODYNAMIQUE OSCILLANT SUPERSONIQUEDANIELS PG.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 3; PP. 541-557; BIBL. 25 REF.Article

CALCUL D'UN ECOULEMENT DECOLLE AUTOUR D'UNE AILE MINCE D'ENVERGURE FINIEBELOTSERKOVSKIJ SM; NISHT MI; SOKOLOVA ON et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 107-112; BIBL. 8 REF.Article

INFLUENCE DES PERTURBATIONS DE TRAINEE SUR LE DEVELOPPEMENT DU DECOLLEMENT DE L'ECOULEMENT A LA BASE DES AUBES DANS LES ETAGES DES TURBINESKIRILLOV II; SHPENZER GG.1977; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1977; VOL. 20; NO 8; PP. 66-70; BIBL. 3 REF.Article

DYNAMIC EFFECTS OF SHOCK-INDUCED FLOW SEPARATION.ERICSSON LE.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 2; PP. 86-92; BIBL. 41 REF.Article

SIMULATION MATHEMATIQUE D'UN ECOULEMENT DECOLLE AUTOUR D'UN PROFIL D'AILE ET DE LA RUPTURE D'UNE NAPPE TOURBILLONNAIRE DANS UN FLUIDE PARFAITAPARINOV VA; BELOTSERKOVSKIJ SM; NISHT MI et al.1976; DOKL. AKAD. NAUK S.S.S.R.; S.S.S.R.; DA. 1976; VOL. 227; NO 4; PP. 820-823; BIBL. 5 REF.Article

SEPARATION AND REATTACHMENT NEAR THE LEADING EDGE OF A THIN AIRFOIL AT INCIDENCECEBECI T; STEWARTSON K; WILLIAMS PG et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 20.1-20.13; BIBL. 25 REF.Article

ANALYTICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF HIGHLY SWEPT WINGS WITH SEPARATED FLOWREDDY CS.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 1; PP. 58-59; BIBL. 9 REF.Article

HYSTERESIS ZONE OR LOCUS-AERODYNAMIC OF BULBOUS BASED BODIES AT LOW SPEEDSCOVERT EE.1979; A.I.A.A.J., NEW YORK; USA; DA. 1979; VOL. 17; NO 6; PP. 659-661; BIBL. 4 REF.Article

PARAMETRES LIMITES DES CARACTERISTIQUES DE DEBIT DES ETAGES DE TURBINEABLAMSKIJ VA.1978; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; BYS; DA. 1978; VOL. 21; NO 9; PP. 81-85; BIBL. 5 REF.Article

INTERACTION VISQUEUSE AVEC DECOLLEMENT EN ECOULEMENT TRANSSONIQUE.DELERY J; CHATTOT JJ; LE BALLEUR JC et al.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 27.1-27.13; ABS. ANGL.; BIBL. 23 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

ETUDE DE L'ECOULEMENT DANS LES ZONES DE DECOLLEMENT DEVANT DES JETS SUPERSONIQUES DANS UN ECOULEMENT SUBSONIQUEAVDUEVSKIJ VS; KRYUKOV VN; OSIPOV YU A et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 64-70; BIBL. 2 REF.Article

MECANISME DE FORMATION DE LA FORCE NORMALE DANS LE BATTEMENT DES AILESBELOTSERKOVSKIJ SM; GULYAEV VV; NISHT MI et al.1974; IN: IZBR. PROBL. PRIKL. MEKH. SB. RAB. POSVYASHCH. SHESTIDESYATILETIYU AKAD. VLADIMIRA NIKOLAEVICHA CHELOMEYA; MOSKVA; VINITI; DA. 1974; PP. 97-102; BIBL. 8 REF.Book Chapter

ECOULEMENT A DECOLLEMENT SUR UNE AILE D'ENVERGURE INFINIE ET A DEBORDEMENT DANS UN FLUIDE PARFAITZUBTSOV AV; SUDAKOV GG.1982; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 3; PP. 65-72; BIBL. 6 REF.Article

VORTEX-LATTICE METHOD FOR THE CALCULATION OF THE NONSTEADY SEPARATED FLOW OVER DELTA WINGSLEVIN D; KATZ J.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 12; PP. 1032-1037; BIBL. 21 REF.Article

MODELES DES ECOULEMENTS A DECOLLEMENT ET PROBLEMES DU CALCUL DES ETAGES DE TURBINEABLAMSKIJ VA.1980; ENERGO-MASHINOSTR.; SUN; DA. 1980; NO 8; PP. 2-4; BIBL. 14 REF.Article

EFFET DU RAPPORT DCP/L D'UNE GRILLE ANNULAIRE SUR LA FORMATION DU DOMAINE DE DECOLLEMENT D'UN ECOULEMENT TOURNANTGOLOSHCHAPOV VN.1976; PROBL. MASHINOSTR., U.S.S.R.; S.S.S.R.; DA. 1976; NO 3; PP. 98-104; BIBL. 3 REF.Article

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