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Results 1 to 25 of 181360

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REGULAR SIMPLE WAVE INTERACTIONS.BURNAT M.1975; ARCH. MECH.; POLAND; DA. 1975; VOL. 27; NO 1; PP. 49-78; ABS. POL. RUSSE; BIBL. 17 REF.Article

STEADY AND OSCILLATORY SUBSONIC AND SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATIONS.MORINO L; LEE TZONG CHEN; SUCIU EO et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 3; PP. 368-374; BIBL. 28 REF.Article

ONE DIMENSIONAL MODELS FOR TRANSIENT GAS-LIQUID FLOWS IN DUCTSHANCOX WT; FERCH RL; LIU WS et al.1980; INTERNATION. J. MULTIPHASE FLOW; GBR; DA. 1980; VOL. 6; NO 1-2; PP. 25-40; BIBL. 21 REF.Article

ON THE UNIQUENESS OF TRANSVERSE MHD FLOWS WITH SAME STREAMLINE PATTERN.NATH VI.1975; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1975; VOL. 28; NO 1; PP. 184-189; BIBL. 5 REF.Article

PREDICTION OF TURBULENT SEPARATED FLOW AT SUBSONIC AND TRANSONIC SPEEDS INCLUDING UNSTEADY EFFECTS. = CALCUL DE L'ECOULEMENT TURBULENT DECOLLE AUX VITESSES SUBSONIQUES ET TRANSSONIQUES, COMPTE TENU DES EFFETS INSTATIONNAIRESKUHN GD; NIELSEN JN.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 26.1-26.16; BIBL. 1 P.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

A CONTINUOUS PREDICTION METHOD FOR FULLY DEVELOPED LAMINAR, TRANSITIONAL, AND TURBULENT FLOWS IN PIPES.WILSON NW; AZAD RS.1975; J. APPL. MECH.; U.S.A.; DA. 1975; VOL. 42; NO 1; PP. 51-54; BIBL. 5 REF.Article

MOUVEMENT STATIONNAIRE NON ISOTHERME D'UN GAZ REEL DANS UNE LONGUE CONDUITE, EN TENANT COMPTE DE L'INFLUENCE DE LA PENTEBABADZHANYAN GA.1975; IZVEST. AKAD. NAUK ARM. S.S.R., MEKH.; S.S.S.R.; DA. 1975; VOL. 28; NO 3; PP. 47-53; ABS. ARM. ANGL.; BIBL. 4 REF.Article

ANALYSE DES ETATS INSTATIONNAIRES DANS DES CONDUITES DANS DES CONDITIONS D'ECOULEMENT FORCEROHATYNSKI R.1976; ARCH. BUDOWY MASZ.; POLSKA; DA. 1976; VOL. 23; NO 2; PP. 179-197; ABS. RUSSE ANGL.; BIBL. 16 REF.Article

LAMINAR GRAVITY-FLOW FILM CONDENSATION OF BINARY VAPOR MIXTURES OF IMMISCIBLE LIQUIDSMARSHALL E; HICKMAN RS.1973; J. HEAT TRANSFER; U.S.A.; DA. 1973; VOL. 95; NO 1; PP. 1-5; BIBL. 8 REF.Serial Issue

EXPERIMENTAL INVESTIGATION OF A TRANSONIC AXIAL FLOW COMPRESSOR STAGE WITH STEADY STATE DISTORTED INLET FLOW.LECHT M; WEYER H.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 4 REF.Conference Paper

A LINEARIZED THEORY OF THREE-DIMENSIONAL AIRFOILS IN NONUNIFORM FLOW.HOMENTCOVSCHI D; BARSONY NAGY A.1976; ACTA MECH.; AUTR.; DA. 1976; VOL. 24; NO 1-2; PP. 63-86; ABS. ALLEM.; BIBL. 9 REF.Article

CALCUL D'UN ECOULEMENT DECOLLE AUTOUR D'UNE AILE MINCE D'ENVERGURE FINIEBELOTSERKOVSKIJ SM; NISHT MI; SOKOLOVA ON et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 107-112; BIBL. 8 REF.Article

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

FLOWFIELD IN THE PLANE OF SYMMETRY BELOW A DELTA WING.CRAMER MS; GEORGE AR; SEEBASS AR et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 2; PP. 212-215; BIBL. 2 REF.Article

TWO-DIMENSIONAL, TWO-PHASE FLOW WITH PHASE TRANSITION IN A DE LAVAL NOZZLE.BRATOS M; BURNAT M.1974; ARCH. MECH.; POLAND; DA. 1974; VOL. 26; NO 6; PP. 965-979; ABS. POL. RUSSE; BIBL. 12 REF.Article

OSCILLATORY FLOW PHENOMENA IN DIFFUSERS IH THE TURBULENT REGIME.PITTALUGA F.1975; MECH. RES. COMMUNIC.; G.B.; DA. 1975; VOL. 2; NO 5-6; PP. 283-288; BIBL. 3 REF.Article

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

FLOW PATTERN TRANSITION FOR GAS-LIQUID FLOW IN HORIZONTAL AND INCLINED PIPES: COMPARISON OF EXPERIMENTAL DATA WITH THEORYBARNEA D; SHOHAM O; TAITEL Y et al.1980; INTERNATION. J. MULTIPHASE FLOW; JPN; DA. 1980; VOL. 6; NO 3; PP. 217-225; BIBL. 1 P.Article

SOME PROBLEMS OF THE THEORY OF CONICAL GAS FLOWS.TESHUKOV VM.1976; ARCH. MECH.; POLAND; DA. 1976; VOL. 28; NO 5-6; PP. 781-786; ABS. POL. ANGL.; BIBL. 4 REF.Article

SOLUTION OF SUBSONIC AXIALLY-SYMMETRIC STREAM FIELDS.FEISTAUER M; RIMANEK J.1975; APL. MAT.; CESKOSL.; DA. 1975; VOL. 20; NO 4; PP. 266-279; ABS. TCHEQUE; BIBL. 4 REF.Article

VISUALISATION DE L'ECOULEMENT DANS UN COMPRESSEUR AXIAL SUPERSONIQUE A AUBES LONGUESFERTIN G.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 3; PP. 165-168; ABS. ANGL.; BIBL. 4REF.Article

SUR UN SCHEMA DE LA METHODE NUMERIQUE DES CARACTERISTIQUES TRIDIMENSIONNELLES POUR LE CALCUL DES ECOULEMENTS IRROTATIONNELS DE GAZAKHMETOV GB; MIKHAJLOV IE.1975; IZVEST. AKAD. NAUK KAZAKH. S.S.R., SER. FIZ.-MAT.; S.S.S.R.; DA. 1975; VOL. 13; NO 3; PP. 29-35; ABS. KAZ.; BIBL. 4 REF.Article

NUMERICAL EXPERIMENTS FOR SUPERSONIC AND HYPERSONIC LOWS.BELOTSERKOVSKII OM; DAVYDOV VM.1974; ACTA ASTRONAUT.; G.B.; DA. 1974; VOL. 1; NO 11-12; PP. 1467-1474; BIBL. 8 REF.; (24TH INT. ASTRONAUT. CONGR.; BAKU, U.S.S.R.; 1973)Conference Paper

REALISATION D'UN PROGRAMME DE CALCUL D'ECOULEMENTS TRIDIMENSIONNELS DE FLUIDES INCOMPRESSIBLES.VIREFLEAU R.1974; DGRST-7270724; FR.; DA. 1974; PP. 1-62; H.T. 50; BIBL. 1 P. 1/2; (RAPP. FINAL, ACTION CONCERTEE: HORS COM.)Report

AN EXPERIMENTAL STUDY OF CHOKED FLOW IN SHORT PIPES WITH LOW AIR WATER MASS FRACTIONS.ILIC V; BRYANT RAA.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 2; PP. 421-423; BIBL. 4 REF.Article

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