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kw.\*:("BOUNDARY LAYER SEPARATION")

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COUCHES LIMITES TURBULENTES TRIDIMENSIONNELLES SUR DES CORPS BIELLIPTIQUES DANS UN ECOULEMENT A ANGLE D'ATTAQUE D'UN GAZ COMPRESSIBLEALEKSIN VA; SHEVELEV YU D.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 39-47; BIBL. 17 REF.Article

INTERACTION D'UNE COUCHE LIMITE TURBULENTE AVEC UN SAUT DE DENSITE A DES VITESSES TRANSONIQUES DE L'ECOULEMENTVELICHKO SA; LIFSHISHCH YU B.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 32-38; BIBL. 17 REF.Article

PHENOMENES D'ECOULEMENT AUTOUR DES FUSELAGES ET DES SYSTEMES AILES-FUSELAGES DES PLANEURSOSTROWSKI J; LITWINCZYK M; TURKOWSKI L et al.1978; ARCH. BUDOWY MASZ.; POLSKA; DA. 1978; VOL. 25; NO 1; PP. 91-104; ABS. RUSSE ANGL.; BIBL. 2 REF.Article

ETUDE EXPERIMENTALE DES ECOULEMENTS DANS LES REGIMES DE SUREXPANSION DANS UNE TUYERE PLATEZATOLOKA VV; ZUDOV VN; SHEVCHENKO VI et al.1978; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1978; NO 1; PP. 39-48; BIBL. 13 REF.Article

INFLUENCE DU DECOLLEMENT DE LA COUCHE LIMITE SUR LA FORMATION DE REGIMES DE MOUVEMENT PARTICULIERS DANS UN SYSTEME COQUE-LIQUIDEKIL'CHEVSKIJ NA; SHAL'DA LM.1978; TEOR. PRILOZH. MEKH.; BGR; DA. 1978; VOL. 8; NO 2; PP. 52-56; BIBL. 3 REF.Article

OPTIMIZATION OF AXI-RADIAL DIFFUSER WALL CONTOURS BASED ON THE SKIN FRICTION COEFFICIENT DISTRIBUTIONHORN SV.1981; AERO-THERMODYNAMICS OF STEAM TURBINES. SYMPOSIUM. AMERICAN SOCIETY OF MECHANICAL ENGINEERS. WINTER ANNUAL MEETING/1981-11-15/WASHINGTON DC; USA; NEW YORK: ASME; DA. 1981; PP. 115-126; BIBL. 18 REF.Conference Paper

BOUNDARY LAYER MEASUREMENTS ON A TWO-DIMENSIONAL WING WITH LAP AND A COMPARISON WITH CALCULATIONSVAN DEN BERG B; OSKAM B.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 271; 14 P.; BIBL. 30 REF.Conference Paper

CALCUL DU FREINAGE SANS DECOLLEMENT D'UN ECOULEMENT EN PRESENCE D'UNE ASPIRATIONBELYANIN NM.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 6; PP. 161-164; BIBL. 7 REF.Article

SOME FEATURES OF UNSTEADY SEPARATING TURBULENT BOUNDARY LAYERSSIMPSON RL; SHIVAPRASAD BG; CHEW YT et al.1981; UNSTEADY TURBULENT SHEAR FLOWS. SYMPOSIUM ON UNSTEADY TURBULENT SHEAR FLOWS/1981/TOULOUSE; DEU/USA; BERLIN; NEW YORK: SPRINGER; DA. 1981; PP. 109-119; BIBL. 11 REF.Conference Paper

ERSCHEINUNGS FORMEN UND AUSWIRKUNGEN VON GRENZSCHICHTABLOESUNGEN IM WASSERBAU = FORMES ET EFFETS DU DECOLLEMENT DE LA COUCHE LIMITE DANS LES CONSTRUCTIONS HYDRAULIQUESINDLEKOFER H; ROUVE G.1980; BAUTECHNIK; DEU; DA. 1980; VOL. 57; NO 4; PP. 122-128; BIBL. 21 REF.Article

QUELQUES EFFETS APPARAISSANT LORS DU CONTROLE DE LA COUCHE LIMITE SUR UNE ZONE DE LA SURFACEGUREVICH YU G; SHAL'MAN E YU.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 4; PP. 3-9; BIBL. 6 REF.Article

MODIFICATIONS OF THE LAW OF THE WALL AND ALGEBRAIC TURBULENCE MODELLING FOR SEPARATED BOUNDARY LAYERS.BALDWIN BS; MACCORMACK RW.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 350; PP. 1-8; BIBL. 16 REF.Conference Paper

VORGANG DES GRENZSCHICHTUMSCHLAGES IN LAMINAREN ABLOESEWIRBELN UND SEINE BERUECKSICHTIGUNG BEI GRENZSCHICHTRECHNUNGEN = LE PROCESSUS DE TRANSITION DE COUCHE LIMITE DANS DES TOURBILLONS DE DECOLLEMENT LAMINAIRES ET SA PRISE EN CONSIDERATION DANS LES CALCULS DE COUCHES LIMITESRANNACHER J.1982; MASCHINENBAUTECHNIK; ISSN 0025-4495; DDR; DA. 1982; VOL. 31; NO 7; PP. 322-325; ABS. RUS/ENG; BIBL. 11 REF.Article

STABILITY AND SEPARATION OF FREELY INTERACTING BOUNDARY LAYERSRYZHOV OS; ZHUK VL.1981; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1981; NO 141; PP. 360-365; BIBL. 7 REF.Conference Paper

EXPERIMENTAL INVESTIGATION OF SUBSONIC TURBULENT SEPARATED BOUNDARY LAYERS ON AN AIRFOIL.SEETHARAM HC; WENTZ WH JR.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 1; PP. 51-55; BIBL. 14 REF.Article

FEATURES OF A SEPARATING TURBULENT BOUNDARY LAYER IN THE VICINITY OF SEPARATION.SIMPSON RL; STRICKLAND JH; BARR PW et al.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 79; NO 3; PP. 553-594; BIBL. 1 P. 1/2Article

INFLUENCE DE LA COURBURE DE LA SECTION TRANSVERSALE DE LA SURFACE SUR LE DECOLLEMENT DE LA COUCHE LIMITEBAM ZELIKOVICH GM.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 4; PP. 80-89; BIBL. 11 REF.Article

BOUNDARY-LAYER SEPARATION ON MOVING WALLS USING AN INTEGRAL THEORY.FANSLER KS; DANBERG JE.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 2; PP. 274-276; BIBL. 14 REF.Article

REATTACHEMENT OF A BLOWNOFF SUPERSONIC BOUNDARY LAYER SUBSEQUENT TO INJECTION CUTOFF.AMR A; KASSOY DR.1976; PHYS. OF FLUIDS; U.S.A.; DA. 1976; VOL. 19; NO 9; PP. 1312-1318; BIBL. 10 REF.Article

THE THEORY OF LAMINAR BOUNDARY LAYER WITH A SEPARATED BUBBLE.STYCZEK A.1976; BULL. ACAD. POLON. SCI., SCI. TECH.; POLOGNE; DA. 1976; VOL. 24; NO 7-8; PP. 605-610; ABS. RUSSE; BIBL. 2 REF.Article

ETUDE DU STADE INITIAL DU DETACHEMENT D'UNE COUCHE LIMITE PAR UNE METHODE D'ELECTRODIFFUSIONKASHINSKIJ ON; MALKOV VA; MUKHIN VA et al.1976; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1976; VOL. 263; NO 8; PP. 29-33; BIBL. 9 REF.Article

CORRELATION OF THE DETACHMENT OF TWO-DIMENSIONAL TURBULENT BOUNDARY LAYERSKLINE SJ; BARDINA JG; STRAWN RC et al.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 68-73; BIBL. 31 REF.Article

EXPERIMENTAL INVESTIGATIONS ON THE VIBRATION OF BLADES DUE TO A ROTATING STALLISHIHARA K; FUNAKAWA M.1980; BULL. ISME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 177; PP. 353-360; BIBL. 8 REF.Article

SEPARATION AHEAD OF PROTUBERANCES IN SUPERSONIC TURBULENT BOUNDARY LAYERS.SEDNEY R; KITCHENS CW JR.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 546-552; BIBL. 15 REF.Article

ANALYSIS OF SEPARATED BOUNDARY-LASER FLOWSCARTER JE; VATSA VN.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 167-174; BIBL. 15 REF.Conference Paper

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