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ROLE OF LAMINAR SEPARATION BUBBLES IN AIRFOIL LEADING-EDGE STALLSVAN DEN BERG B.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 553-556; BIBL. 18 REF.Article

COMPARISON OF SHOCK-INDUCED TWO- AND THREE-DIMENSIONAL INCIPIENT TURBULENT SEPARATION.KORREGI RH.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 534-535; BIBL. 16 REF.Article

INVESTIGATION OF THE THREE-DIMENSIONAL BOUNDARY LAYER SEPARATION CRITERIA BY A MINIMUM PRINCIPLE.WARSI ZUA.1975; INTERNATION. J. ENGNG SCI.; G.B.; DA. 1975; VOL. 13; NO 2; PP. 161-171; BIBL. 10 REF.Article

PARAMETRES DU SECOND ORDRE INTERVENANT DANS LE DECOLLEMENT D'UNE COUCHE LIMITE TRIDIMENSIONNELLEBAM ZELIKOVICH GM.1974; PRIKL. MAT. MEKH.; S.S.S.R.; DA. 1974; VOL. 38; NO 4; PP. 666-674; BIBL. 4 REF.Article

THE INITIATION OF GASEOUS MICROBUBBLE GROWTH IN LAMINAR SEPARATION BUBBLESPARKIN BR.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 4; PP. 543-550; BIBL. 12 REF.Article

BOUNDARY LAYER OVER A BLUNT BODY AT HIGH INCIDENCE WITH AN OPEN-TYPE OF SEPARATION.WANG KC.1974; PROC. R. SOC. LONDON, A; G.B.; DA. 1974; VOL. 340; NO 1620; PP. 33-55; BIBL. 19 REF.Article

A POSSIBLE CRITERION FOR CAVITATION INCEPTION ON HEMISPHERICAL HEADFORMSPARKIN BR.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 4; PP. 577-582; BIBL. 18 REF.Article

CAVITATION INCEPTION OBSERVATIONS ON AXISYMMETRIC BODIES AT SUPERCRITICAL REYNOLDS NUMBERS.ARAKERI VH; ACOSTA AJ.1976; J. SHIP RES.; U.S.A.; DA. 1976; VOL. 20; NO 1; PP. 40-50; BIBL. 21 REF.Article

BULBE DE DECOLLEMENT LAMINAIRE AVEC TRANSITION: ESSAI DE PREVISION AVEC COUPLAGE LOCALGLEYZES C; COUSTEIX J; BONNET JL et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 21.1-21.16; ABS. ENG; BIBL. 18 REF.Article

FINITE DIFFERENCE SOLUTIONS FOR SUPERSONIC SEPARATED FLOWS. = SOLUTIONS AUX DIFFERENCES FINIES POUR LES ECOULEMENTS SUPERSONIQUES DECOLLESWERLE MJ; POLAK A; VATSA VN et al.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 8.1-8.12; BIBL. 25 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

ANALYSIS OF FLOW SEPARATION IN AN ANNULAR EXPANSION-CONTRACTION WITH INNER CYLINDER ROTATING.DAILEY GF; GEIGER GE.1973; J. FLUIDS ENGNG; U.S.A.; DA. 1973; VOL. 95; NO 4; PP. 485-492; BIBL. 10 REF.Article

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

COMBINED CHOROIDAL AND RETINAL DETACHMENTGOTTLIEB F.1972; ARCH. OPHTHALMOL.; U.S.A.; DA. 1972; VOL. 88; NO 5; PP. 481-486; BIBL. 15REF.Serial Issue

DE L'ILLUSION DUE A L'ASPECTPRONIER H.1972; TECHNICUIR; FR.; DA. 1972; VOL. 6; NO 9; PP. 176Serial Issue

NEW DIAGNOSTIC TECHNIQUE FOR THE STUDY OF TURBULENT BOUNDARY-LAYER SEPARATION.HORSTMAN CC; OWEN FK.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1437-1438; BIBL. 4 REF.Article

CHOROIDAL DETACHMENT FOLLOWING RETINAL DETACHMENT SURGERY WITHOUT DRAINAGE OF SUBRETINAL FLUID = DECOLLEMENT CHOROIDIEN APRES TRAITEMENT CHIRURGICAL DU DECOLLEMENT DE RETINE SANS DRAINAGE DU LIQUIDE SOUS-RETINIENCHIGNELL AH.1972; AMER. J. OPHTHALMOL.; U.S.A.; DA. 1972; VOL. 73; NO 6; PP. 860-862; BIBL. 7REF.Serial Issue

NAISSANCE DE ZONES DE DECOLLEMENT DANS DES ETAGES DE TURBINE A GRAND ETALEMENTBOGOMOLOVA TV.1975; TEPLOENERGETIKA; S.S.S.R.; DA. 1975; NO 9; PP. 77-79; BIBL. 4 REF.Serial Issue

CONTRIBUTION A L'ETUDE DU DECOLLEMENT TRIDIMENSIONNEL.MOREY JC; ZUBER G.1974; AERONAUT. ET ASTRONAUT.; FR.; DA. 1974; NO 46; PP. 31-39; ABS. ANGL. ALLEM.; BIBL. 15 REF.Article

TECHNICAL EVALUATION REPORT ON THE FLUID DYNAMICS PANEL SYMPOSIUM ON FLOW SEPARATION.PEAKE DJ; RAINBIRD WJ.1976; AGARD-AR-98; FR.; DA. 1976; PP. (16P.); BIBL. 2 P.; ISBN 928351226X; (AGARD FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Report

SOME PRACTICAL ASPECTS OF THE BURST OF LAMINAR SEPARATION BUBBLESKAMIYA N; SUZUKI S; NAKAMURA M et al.sdICAS 1980. INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES. CONGRESS. 12/1980/MUNICH; USA; DA. S.D.; PP. 417-428; BIBL. 15 REF.Conference Paper

WIDERSTANDSVERMINDERUNG DURCH BLASTURBULATOREN = REDUCTION DE TRAINEE PAR DES TURBULATEURSHORSTMANN KH; QUAST A.1981; FORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT-RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1981; NO 33; PP. 1-53; ABS. ENG; BIBL. 20 REF.Article

LAMINAR BOUNDARY LAYER OVER A BODY OF REVOLUTION AT EXTREMELY HIGH INCIDENCE.WANG KC.1974; PHYS. OF FLUIDS; U.S.A.; DA. 1974; VOL. 17; NO 7; PP. 1381-1385; BIBL. 8 REF.Article

DECOLLEMENT D'UNE BULLE DE VAPEUR ET CALCUL DU RAYON DE DECOLLEMENTFEDOTKIN IM; KONSTANTINOV SM; TERESHCHENKO AA et al.1973; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1973; VOL. 24; NO 5; PP. 831-835; ABS. ANGL.; BIBL. 15 REF.Serial Issue

CALCULATION OF LAMINAR SEPARATION BUBBLES AND THEIR EFFECT ON AIRFOIL PERFORMANCEROBERTS WB.1980; A.I.A.A. J. NEW YORK; USA; DA. 1980; VOL. 18; NO 1; PP. 25-31; BIBL. 20 REF.Article

A NOTE ON THE EFFECT OF SHORT AND LONG LAMINAR SEPARATION BUBBLES ON DESINENT CAVITATIONARAKERI VH; CARROLL JA; HOLL JW et al.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 1; PP. 28-32; BIBL. 10 REF.Article

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