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Results 1 to 25 of 1634

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A wind tunnel inlet flow simulationKAUL, U. P.Journal of aircraft. 1985, Vol 22, Num 10, pp 927-928, issn 0021-8669Article

A FLOW STUDY IN RADIAL INFLOW TURBINE SCROLL-NOZZLE ASSEMBLY.HAMED A; BASKHARONE E; TABAKOFF W et al.1978; J. FLUIDS ENGNG; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 31-36; BIBL. 21 REF.Article

STABILITY OF AN AXIAL FLOW COMPRESSOR WITH STEADY INLET CONDITIONS.CORBETT AG; ELDER RL.1974; J. MECH. ENGNG SCI.; G.B.; DA. 1974; VOL. 16; NO 6; PP. 377-385; BIBL. 8 REF.Article

ENTRANCE REGION HEAT TRANSFER BETWEEN PARALLEL PLATES WITH UNIFORM WALL TEMPERATURELOU YS; BARTON LO.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 393-394; BIBL. 5 REF.Serial Issue

Shell-side distribution and the influence of inlet conditions in a model of a disc- and -doughnut heat exchangerFOUNTI, M. A; VAFIDIS, C; WHITELAW, J. H et al.Experiments in fluids. 1985, Vol 3, Num 5, pp 293-300, issn 0723-4864Article

Ecoulement d'un gaz raréfié dans la cavité d'entrée d'une pompe à diffusionMAKAROV, A. M; PARASHCHENKO, E. V; BOJTSOV, V. I et al.Inženerno-fizičeskij žurnal. 1985, Vol 49, Num 4, pp 682-683, issn 0021-0285Article

Ecoulement à l'entrée d'un tube à rebord à arête vive. I. Modèle physique d'écoulementLEGKIJ, V. M; ROGACHEV, V. A.Inženerno-fizičeskij žurnal. 1989, Vol 56, Num 2, pp 215-220, issn 0021-0285Article

Inlet reverse flow mechanism in axial flow turbomachines with neither stall nor significant radial flowAOKI, M; YAMAMOTO, K.Journal of turbomachinery. 1992, Vol 114, Num 2, pp 392-397, issn 0889-504XArticle

An analytical investigation of the ground and ambient head flow influence on the free inlet flow into a turbojet engineGAJEWSKI, T.Journal of Technical Physics. 1984, Vol 25, Num 2, pp 229-240, issn 0324-8313Article

THE PRANDTL NUMBER DEPENDENCE OF THE CONVECTIVE HEAT TRANSFER COEFFICIENT IN A TURBULENT THERMAL ENTRANCE REGIONEISSENBERG DM; DAY JT; PORTAL C et al.1973; A.I. CH. E.J., NEW YORK; U.S.A.; DA. 1973; VOL. 19; NO 2; PP. 393-394; BIBL. 4 REF.Serial Issue

HEAT TRANSFER FOR DEVELOPING LAMINAR FLOW IN THE ENTRANCE OF A TUBEROY DN.1968; J. INSTIT. ENGRS (INDIA), MECH. ENGNG DIV.; INDIA; DA. 1968; VOL. 49; NO 1; PP. 71-79; BIBL. 18 REF.Serial Issue

Computational method for screened two-dimensional wind tunnel inletsCOIRIER, W. J; BRAGG, M. B.Journal of aircraft. 1987, Vol 24, Num 4, pp 281-283, issn 0021-8669Article

Turbulenzstruktur im Wandkanal eines Stabbündels (P/D=W/D=1.148) für drei Ebenen im Einlauf = Structure turbulente dans le canal pariétal d'un faisceau de barres (P/D=W/D=1,148) dans trois plans dans l'entrée = Structure of turbulence in a wall subchannel of a rod bundle (P/D=W/D=1,148) in three axial planes downstream of the entranceREHME, K.Kernforschungszentrum Karlsruhe. 1986, Num 4027, issn 0303-4003, 77 p.Serial Issue

Effects of small-scale, high intensity inlet turbulence on flow in a two-dimensional diffuserHOFFMANN, J. A; GONZALEZ, G.Journal of fluids engineering. 1984, Vol 106, Num 2, pp 121-124, issn 0098-2202Article

Centrifugal fan performance with distorted inflowsWRIGHT, T; MADHAVAN, S; DI RE, J et al.Journal of engineering for gas turbines and power. 1984, Vol 106, Num 4, pp 895-900, issn 0742-4795Article

A note on the mass transfer in the entrance to a flat duct with permeable wallsINGHAM, D. B.International journal of heat and mass transfer. 1984, Vol 27, Num 12, pp 2421-2422, issn 0017-9310Article

Diffusive, electrostatic, and gravitational deposition of suspensions in the entrance of a nozzleKORJACK, T. A.Journal of applied mechanics. 1983, Vol 50, Num 1, pp 1-7, issn 0021-8936Article

Etude physique et simulation numérique des écoulements dans les entrées d'air supersoniques = Physical aspects and numerical simulation of the flows in supersonic air-intakesFreskos, Grigorids; Ha Minh, Hieu.1992, 256 p.Thesis

Etude des configurations d'un jet d'eau d'entrée. IIKASHIWADANI, T.Journal of the Society of Naval Architects of Japan. 1986, Vol 159, pp 118-128, issn 0514-8499Article

Flow development in a porous channel and tubeBRADY, J. F.The Physics of fluids. 1984, Vol 27, Num 5, pp 1061-1067, issn 0031-9171Article

Turbulent heat transfer coefficients in an isothermal-walled tube for either a built-in or free inletSPARROW, E. M; MOLKI, M.International journal of heat and mass transfer. 1984, Vol 27, Num 5, pp 669-675, issn 0017-9310Article

Determination of the transmission efficiency of an aircraft aerosol inletHEGG, Dean A; COVERT, David S; JONSSON, Haflidi et al.Aerosol science and technology. 2005, Vol 39, Num 10, pp 966-971, issn 0278-6826, 6 p.Article

Transition vers la turbulence dans la partie initiale d'un tuyau circulaireKOLYADA, V. V; PAVEL'EV, A. A.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1985, Num 4, pp 52-56, issn 0568-5281Article

InletsHINSHAW, J.LC GC. 1987, Vol 5, Num 11, pp 954-960, issn 0888-9090, 4 p.Article

Transfert de chaleur dans la longueur d'entrée thermique dans un écoulement laminaire de film tombant avec des conditions aux limites du troisième ordreSOBIN, V. M; KRAVCHENKO, V. A.Inženerno-fizičeskij žurnal. 1986, Vol 50, Num 1, pp 133-134, issn 0021-0285Article

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