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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

DIRECT APPROACH TO AERODYNAMIC DESIGN PROBLEMSCHIN WC.1981; J. APPL. MECH.; ISSN 0021-8936; USA; DA. 1981; VOL. 48; NO 4; PP. 721-726; BIBL. 11 REF.Article

A REVIEW OF SEPARATION IN STEADY, THREE-DIMENSIONAL FLOW. = REVUE DU DECOLLEMENT EN ECOULEMENT TRIDIMENSIONNEL STATIONNAIRESMITH JHB.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 31.1-31.17; BIBL. 4 P.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

FLOW PATTERN TRANSITIONS IN VERTICAL AND UPWARDLY INCLINED LINESWEISMAN J; KANG SY.1981; INT. J. MULTIPH. FLOW; ISSN 0301-9322; GBR; DA. 1981; VOL. 7; NO 3; PP. 271-291; BIBL. 20 REF.Article

THREE-DIMENSIONAL, SHOCK-ON-SHOCK INTERACTION PROBLEM.KUTLER P; SAKELL L.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1360-1367; BIBL. 32 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

CONDITIONS DE PRODUCTION D'UN ECOULEMENT CRITIQUE DES GAZ A TRAVERS DES CORPS POREUXBELOV SV; KARTUESOV OG; NOVIKOV YU M et al.1976; TEPLOENERGETIKA; S.S.S.R.; DA. 1976; NO 2; PP. 41-43; BIBL. 5 REF.Article

ISOMETRIC MOTION IN RELATIVISTIC MAGNETOHYDRODYNAMICSCIUBOTARIU CD.1972; PHYS. LETTERS, A; NETHERL.; DA. 1972; VOL. 40; NO 5; PP. 369-370; BIBL. 6 REF.Serial Issue

RECHENANSAETZE FUER DAS STROEMUNGSFELD IN KONVERGIEREND-DIVERGIERENDEN DRALLDUESEN. = PRINCIPES POUR LE CALCUL DU CHAMP D'ECOULEMENT DANS DES TUYERES CONVERGENTES-DIVERGENTES A ECOULEMENT ROTATIONNELCOLDITZ M.1974; FORSCH. IM. INGR-WES.; DTSCH.; DA. 1974; VOL. 40; NO 3; PP. 81-86; ABS. ANGL.; BIBL. 20 REF.Article

STAND DER ERKENNTNIS UND BEDEUTUNG DER ZWEIPHASENSTROEMUNG IM WAERMETECHNISCHEN APPARATEBAU = ETAT DES CONNAISSANCES ET IMPORTANCE DE L'ECOULEMENT DIPHASIQUE EN THERMIQUEHERRMANN W.1972; ENERGIETECHNIK; DTSCH.; DA. 1972; VOL. 22; NO 8; PP. 331-336; BIBL. 15 REF.Serial Issue

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

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