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ANALYSIS OF A TURBULENT BOUNDARY LAYER SUBJECTED TO A STRONG ADVERSE PRESSURE GRADIENTNOOR AFZAL.1983; INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE; ISSN 0020-7225; GBR; DA. 1983; VOL. 21; NO 6; PP. 563-576; BIBL. 21 REF.Article

EQUILIBRIUM BOUNDARY LAYERS IN MODERATE TO STRONG ADVERSE PRESSURE GRADIENTSSCHOFIELD WH.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981-12; VOL. 113; PP. 91-122; BIBL. 34 REF.Article

HEAT TRANSFER IN TURBULENT FLOWS UNDER MILD AND STRONG ADVERSE PRESSURE GRADIENT CONDITIONS FOR AN ARBITRARY VARIATION OF THE WALL TEMPERATURE. = TRANSFERT DE CHALEUR DANS DES ECOULEMENTS TURBULENTS DANS DES CONDITIONS DE GRADIENT DE PRESSION MOYENNEMENT ET FORTEMENT DEFAVORABLE POUR UNE VARIATION ARBITRAIRE DE LA TEMPERATURE DE PAROIORLANDO AF; MOFFAT RJ; KAYS WM et al.1974; IN: HEAT TRANSFER FLUID MECH. INST. 24TH MEET. PROC.; CORVALLIS, OREG.; 1974; STANFORD, CALIF.; STANFORD UNIV.; DA. 1974; PP. 91-104; BIBL. 7 REF.Conference Paper

INVESTIGATION OF PARAMETERS OF A TURBULENT BOUNDARY LAYER IN AN ADVERSE PRESSURE GRADIENTZUKAUSKAS AA; ULINSKAS RV.1981; HEAT TRANSFER. SOVIET RESEARCH; ISSN 0440-5749; USA; DA. 1981 PUBL. 1982; VOL. 13; NO 5; PP. 25-35; BIBL. 10 REF.Article

TRANSITION D'UNE COUCHE LIMITE TURBULENTE EN COUCHE LAMINAIRE A DES GRADIENTS DE PRESSION FAVORABLES ELEVESREPIK EU.1973; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1973; VOL. 24; NO 2; PP. 276-281; ABS. ANGL.; BIBL. 9 REF.Serial Issue

ALVEOLAR-ARTERIAL OXYGEN TENSION DIFFERENCE: A CRITICAL LOOKTORDA TA.1981; ANAESTH. INTENSIVE CARE; ISSN 0310-057X; AUS; DA. 1981; VOL. 9; NO 4; PP. 326-330; BIBL. 6 REF.Article

GRADIENTS DE PRESSION DANS LES ZONES ETROITES D'UN FRONT FROIDMASTERSKIKH MA.1980; METEOROL. I GIDROL.; SUN; DA. 1980; NO 8; PP. 102-104; BIBL. 6 REF.Article

THE CAVITATION CHARACTERISTICS OF MAU-TYPE PROPELLER. II: PRESSURE DISTRIBUTION ON BLADE SURFACE IN NON-UNIFORM FLOW.TAKAHASHI M; OKU M.1978; J. SOC. NAV. ARCHITECTS JAP.; JPN; DA. 1978; VOL. 143; PP. 61-68; ABS. ENG; BIBL. 7 REF.Article

TURBULENT AIRFOILS FOR GENERAL AVIATION.EPPLER R.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 93-99; BIBL. 21 REF.Article

ETUDE DE LA REPARTITION DES PRESSIONS DANS DES SILOS METALLIQUES A GRAINS DU TYPE A MEMBRANE ET CARCASSEKISELEV BE; BARANOV DS; KHOROSHIJ IS et al.1978; STROITEL. MEKH. RASCHET SOORUZH.; S.S.S.R.; DA. 1978; NO 2; PP. 75-76; BIBL. 5 REF.Article

SECOND-ORDER GRADIENT UNIDIRECTIONAL MICROPHONES UTILIZING AN ELECTRET TRANSDUCER.SESSLER GM; WEST JE.1975; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1975; VOL. 58; NO 1; PP. 273-279; BIBL. 12 REF.Article

EVOLUTION OF A MODERATELY SHORT TURBULENT BOUNDARY LAYER IN A SEVERE PRESSURE GRADIENT.DEISSLER RG.1974; J. FLUID MECH.; G.B.; DA. 1974; VOL. 64; NO 4; PP. 763-774; BIBL. 11 REF.Article

PRESSURE FLUCTUATIONS IN SUBMERGED JUMP. = FLUCTUATIONS DE LA PRESSION D'UN RESSAUT SUBMERGENARASIMHAN S; BHARGAVA VP.1976; PROC. AMER. SOC. CIV. ENGRS, J. HYDRAUL. DIV.; U.S.A.; DA. 1976; VOL. 102; NO HY3; PP. 339-350; BIBL. 8REF.Article

TURBULENT WAKE BEHAVIOR WITH AXIAL PRESSURE GRADIENTS. = COMPORTEMENT DU SILLAGE TURBULENT AVEC DES GRADIENTS DE PRESSION AXIAUXPITTALUGA F.1975; MECH. RES. COMMUNIC.; G.B.; DA. 1975; VOL. 2; NO 5-6; PP. 261-266; BIBL. 7 REF.Article

EVALUATION OF THE TURBULENT TRANSPORT TERMS FOR A TWO-DIMENSIONAL NOZZLE WALL BOUNDARY-LAYER FLOW AT MACH 5 AND WITH PRESSURE GRADIENT, HEAT TRANSFER AND UPSTREAM EFFECTS.LEE RE; SMITH RA.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 96; PP. 1-14; BIBL. 43 REF.Conference Paper

PATHWAYS FOR BULK OUTFLOW OF AQUEOUS HUMOUR AND CEREBROSPINAL FLUIDTRIPATHI BJ; TRIPATHI RC.1974; J. PHYSIOL.; G.B.; DA. 1974; VOL. 240; NO 2; PP. 4P-6P; BIBL. 5REF.Article

AN IMPROVEMENT TO AN ALGORITHM FOR COMPUTING AIRCRAFT REFERENCE ALTITUDEBLANCHARD RL.1972; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1972; VOL. 8; NO 5; PP. 685-687; BIBL. 4 REF.Serial Issue

THE PREDICTION OF TURBULENT BOUNDARY LAYER PARAMETERS IN CONICAL DIFFUSEUR FLOWS.WIRASINGHE NEA; NEVE RS.1974; AERONAUT. QUART.; G.B.; DA. 1974; VOL. 25; NO 3; PP. 199-209; BIBL. 6 REF.Article

DESIGN OF DRIP IRRIGATION MAIN LINESI PAI WU.1975; PROC. AMER. SOC. CIV. ENGR., J. IRRIG. DRAIN. DIV.; U.S.A.; DA. 1975; VOL. 101; NO 4; PP. 265-278; BIBL. 9 REF.Article

DIRECTIVAS PARA A COLOCAO DAS COMPORTAS NOS DESCARREGADORES DAS BARRAGENS = DIRECTIVES POUR LA SITUATION DES VANNES DANS LES DEVERSOIRRS DE BARRAGESDE OLIVEIRA LEMOS F.1975; LAB. NACION. ENGRIA CIV., MEM.; PORTUG.; DA. 1975; NO 469; PP. 1-18; ABS. ANGL.; BIBL. 5REF.Serial Issue

STUDY OF THE OXYGENATION OF CARDIAC PATIENTS SUBMITTED TO EXTRACORPOREAL CIRCULATION = ETUDE DE L'OXYGENATION DES MALADES CARDIAQUES SOUMIS A UNE CIRCULATION EXTRACORPORELLEBARAT G; DOMINGUEZ DE VILLOTA E; AVELLO F et al.1972; BRIT. J. ANAESTH.; G.B.; DA. 1972; VOL. 44; NO 8; PP. 817-825; ABS. FR. ALLEM. ESP.; BIBL. 22REF.Serial Issue

THE COMPONENTS OF THE ALVEOLAR-ARTERIAL OXYGEN TENSION DIFFERENCE IN NORMAN SUBJECTS AND IN PATIENTS WITH PNEUMONIA AND OBSTRUCTIVE LUNG DISEASE = FACTEURS DE LA DIFFERENCE DE PRESSION D'OXYGENE ALVEOLO-ARTERIEL CHEZ LES GENS NORMAUX ET CHEZ LES MALADES ATTEINTS DE PNEUMONIE ET D'AFFECTIONS PULMONAIRES OBSTRUCTIVESDAVIDSON FF; GLAZIER JB; MURRAY JF et al.1972; AMER. J. MED.; U.S.A.; DA. 1972; VOL. 52; NO 6; PP. 754-762; BIBL. 25REF.Serial Issue

DIFFRACTION CONSTANTS FOR PRESSURE GRADIENT TRANSDUCERSWOOLLETT RS.1982; JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA; ISSN 0001-4966; USA; DA. 1982; VOL. 72; NO 4; PP. 1105-1113; BIBL. 18 REF.Article

PRESSURE OVERRIDE SYSTEM PROVIDES WIDE RANGE CONTROLLABILITY.MARCUS DN.1978; PIPE LINE INDUSTRY; U.S.A.; DA. 1978; VOL. 48; NO 1; PP. 69-71; BIBL. 1 REF.Article

SPALTFUELLUNG - EIN LAGERPROBLEM. = FILM COMPLET - UN PROBLEME DE PALIER.MAAS H.1977; SCHMIERTECH. U. TRIBOL.; DTSCH.; DA. 1977; VOL. 24; NO 5; PP. 130-133; BIBL. 5 REF.Article

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