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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

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

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

SEPARATED FLOW OVER A BODY OF REVOLUTION.MARSHALL FJ; DEFFENBAUGH FD.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 2; PP. 78-85; BIBL. 31 REF.Article

TRANSONIC LAMINAR VISCOUS-INVISCID INTERACTION OVER AIRFOILS.TAI TC.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 1065-1072; BIBL. 29 REF.Article

VERIFICATION EXPERIMENTALE DES CARACTERISTIQUES DE PROFILS D'AUBES DE TURBOMACHINES.PLUVIOSE M.1975; DGRST-7371247; FR.; DA. 1975; PP. (60P.); BIBL. 12 REF.; (RAPP. FINAL, ACTION CONCERTEE: MEC.)Report

HEAT TRANSFER IN SEPARATED AND REATTACHED FLOWS: AN ANNOTATED REVIEW.FLETCHER LS; BRIGGS DG; PAGE RH et al.1974; ISRAEL J. TECHNOL.; ISRAEL; DA. 1974; VOL. 12; NO 3-4; PP. 236-261; BIBL. 7 P. 1/2; (8TH ISR. CONF. MECH. ENG. PROC.; TECHNION CITY, HAIFA; 1974)Conference Paper

LE TUNNEL HYDRODYNAMIQUE AU SERVICE DE LA RECHERCHE AEROSPATIALE.WERLE H.1974; OFF. NATION. ET. RECH. AEROSPAT., PUBL.; FR.; DA. 1974; NO 156; PP. 1-83; BIBL. 5 P. 1/2Serial Issue

DRY-SURFACE COATING METHOD FOR VISUALIZATION OF SEPARATION ON A BLUFF BODYSADEH WZ; BRAUER HJ; DURGIN JR et al.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 7; PP. 954-956; BIBL. 7 REF.Article

DESIGN OF FLAT PLATE LEADING EDYES TO AVOID FLOW SEPARATIONDAVIS MR.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 598-600; BIBL. 9 REF.Article

COMMENT ON "UNSTEADY SEPARATION PHENOMENA IN A TWO-DIMENSIONAL CAVITY".TELIONIS DP; O'BRIEN V.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1679-1680; BIBL. 14 REF.Article

LAMINAR SEPARATION AT A TRAILING EDGE. = DECOLLEMENT LAMINAIRE A UN BORD DE FUITEGUIRAUD JP; SCHMITT R.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 3.1-3.5; ABS. FR.; BIBL. 11 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

QUELQUES PROBLEMES D'AEROELASTICITE DANS LE CAS D'UN ECOULEMENT DECOLLEBELOTSERKOVSKIJ SM; VOL'MIR AS; NISHT MI et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. TVERD. TELA; S.S.S.R.; DA. 1975; NO 5; PP. 150-157; BIBL. 9 REF.Article

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