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AN UNSTEADY LAMINAR BOUNDARY LAYER WITH SEPARATION AND REATTACHMENTCEBECI T.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 12; PP. 1305-1306; BIBL. 15 REF.Article

CALCULATION OF UNSTEADY TWO-DIMENSIONAL LAMINAR AND TURBULENT BOUNDARY LAYERS WITH FLUCTUATIONS IN EXTERNAL VELOCITY.CEBECI T.1977; PROC. R. SOC. LONDON, A; G.B.; DA. 1977; VOL. 355; NO 1681; PP. 225-238; BIBL. 18 REF.Article

CALCULATION OF THREE-DIMENSIONAL BOUNDARY LAYERS. I. SWEPT INFINITE CYLINDERS AND SMALL CROSS FLOW.CEBECI T.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 779-786; BIBL. 15 REF.Article

EDDY-VISCOSITY DISTRIBUTION IN THICK AXISYMMETRIC TURBULENT BOUNDARY LAYERSCEBECI T.1972; IN: AM. SOC. MECH. ENG. WINTER ANNU. MEET.; NEW YORK, N.Y.; 1972; S.L.; A.S.M.E.; DA. 1972; VOL. FE-18; PP. 1-6; BIBL. 9 REF.Conference Paper

CALCULATION OF MOMENTUM AND HEAT TRANSFER IN INTERNAL FLOWS AND IN FLOWS WITH SMALL REGIONS OF SEPARATIONCEBECI T.1979; TURBULENT FORCED CONVECTION IN CHANNELS AND BUNDLES. NORTH ATLANTIC TREATY ORGANIZATION ADVANCED STUDY INSTITUTE/1978/ISTANBUL; USA/GBR; WASHINGTON: HEMISPHERE/NEW YORK: HEMISPHERE/LONDON: HEMISPHERE; DA. 1979; VOL. 1; PP. 75-114; BIBL. 54 REF.Conference Paper

ON THE SOLUTION OF LOCAL NONSIMILAR BOUNDARY-LAYER EQUATIONS FOR STANDARD AND INVERSE FLOWS.CEBECI T.1975; LETTERS HEAT MASS TRANSFER; G.B.; DA. 1975; VOL. 2; NO 1; PP. 71-79; BIBL. 12 REF.Article

CALCULATION OF THREE-DIMENSIONAL BOUNDARY LAYERS. II. THREE-DIMENSIONAL FLOWS IN CARTESIAN COORDINATES.CEBECI T.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 1056-1064; BIBL. 19 REF.Article

KINEMATIC EDDY VISCOSITY AT LOW REYNOLDS NUMBERSCEBECI T.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 1; PP. 102-104; BIBL. 13 REF.Serial Issue

MODELLING REQUIREMENTS FOR THE CALCULATION OF THE TURBULENT FLOW AROUND AIRFOILS, WINGS AND BODIES OF REVOLUTIONCEBECI T; MEIER HU.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 271; 12 P.; BIBL. 28 REF.Conference Paper

ON STABILITY AND TRANSITION IN THREE-DIMENSIONAL FLOWSCEBECI T; STEWARTSON K.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 4; PP. 398-405; BIBL. 46 REF.Article

PREDICTION OF TURBULENT BOUNDARY LAYERS ON CONES AT INCIDENCE.KAUPS K; CEBECI T.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 5; PP. 727-730; BIBL. 11 REF.Article

A time-dependent approach for calculating steady inverse boundary-layer flows with separationCEBECI, T.Proceedings of the royal society of London, series A : mathematical and physical sciences. 1983, Vol 389, Num 1796, pp 171-178, issn 0080-4630Article

CALCULATION OF TURBULENT FLOWS.REYNOLDS WC; CEBECI T.1976; TOPICS APPL. PHYS.; GERM.; DA. 1976; VOL. 12; PP. 193-229; BIBL. 1 P.Article

BOUNDARY LAYERS ON A ROTATING DISK.CEBECI T; ABBOTT DE.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 6; PP. 829-832; BIBL. 11 REF.Article

A NOTE ON THE SPECIFICATION OF FREESTREAM VELOCITY IN THE CALCULATION OF THE BOUNDARY LAYER FLOW AROUND BODIES OF REVOLUTION AT INCIDENCECEBECI T; MEIER HU.1982; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1982; VOL. 6; NO 6; PP. 416-418; ABS. GER; BIBL. 6 REF.Article

LAMINAR BOUNDARY LAYERS WITH ASSIGNED WALL SHEARCEBECI T; KELLER HB.1973; LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 79-85; BIBL. 7 REF.; (PROC. 3RD. INT. CONF. NUMER. METHODS FLUID MECH. II. PROBL. FLUID MECH.; PARIS; 1972)Conference Paper

Effect of ice on airfoil stall at high Reynolds numbersCEBECI, T.AIAA journal. 1995, Vol 33, Num 7, pp 1351-1352, issn 0001-1452Article

Calculation of flow over iced airfoilsCEBECI, T.AIAA journal. 1989, Vol 27, Num 7, pp 853-861, issn 0001-1452Conference Paper

Unsteady boundary layers with an intelligent numerical schemeCEBECI, T.Journal of Fluid Mechanics. 1986, Vol 163, pp 129-140, issn 0022-1120Article

PREDICTION OF BOUNDARY LAYER CHARACTERISTICS OF AN OSCILLATING AIRFOILCEBECI T; CARR LW.1981; UNSTEADY TURBULENT SHEAR FLOWS. SYMPOSIUM ON UNSTEADY TURBULENT SHEAR FLOWS/1981/TOULOUSE; DEU/USA; BERLIN; NEW YORK: SPRINGER; DA. 1981; PP. 145-158; BIBL. 13 REF.Conference Paper

CALCULATION OF INCOMPRESSIBLE ROUGH-WALL BOUNDARY LAYER FLOWSCEBECI T; CHANG KC.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 730-735; BIBL. 15 REF.Article

THREE-DIMENSIONAL LAMINAR BOUNDARY LAYERS AND THE OK OF ACCESSIBILITYCEBECI T; KHATTAB AK; STEWARTSON K et al.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 107; PP. 57-87; BIBL. 2 P.Article

ON THE RESPONSE OF A STAGNATION BOUNDARY LAYER TO A CHANGE IN THE EXTERNAL VELOCITYCEBECI T; STEWARTSON K; WILLIAMS PG et al.1979; S.I.A.M. J. APPL. MATH.; USA; DA. 1979; VOL. 36; NO 2; PP. 190-199; BIBL. 6 REF.Article

SOLUTION OF A HYPERBOLIC SYSTEM OF TURBULENCE-MODEL EQUATIONS BY THE "BOX" SCHEMECEBECI T; CHANG KC; BRADSHAW P et al.1980; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1980; VOL. 22; NO 2; PP. 213-227; BIBL. 12 REF.Article

A BOUNDARY-LAYER COLLISION IN A CURVED DUCTSTEWARTSON K; CEBECI T; CHANG KC et al.1980; QUART. J. MECH. APPL. MATH.; GBR; DA. 1980; VOL. 33; NO 1; PP. 59-75; BIBL. 38 REF.Article

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