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Results 1 to 25 of 15114

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CONVECTION DANS UN LIQUIDE CHAUFFE PAR EN DESSOUS DANS UNE ENCEINTE FERMEE, EN TENANT COMPTE DES VARIATIONS DE LA VISCOSITE EN FONCTION DE LA TEMPERATUREGERSHUNI GZ; ZHUKHOVITSKIJ EM; TARUNIN EL et al.1973; TEPLOFIZ. VYS. TEMPER.; S.S.S.R.; DA. 1973; VOL. 11; NO 3; PP. 579-587; BIBL. 13 REF.Serial Issue

UPWIND SECOND-ORDER DIFFERENCE SCHEMES AND APPLICATIONS IN UNSTEADY AERODYNAMIC FLOWS. = SCHEMAS AUX DIFFERENCES FINIES DU SECOND ORDRE ET APPLICATIONS AUX ECOULEMENTS AERODYNAMIQUES INSTATIONNAIRESWARMING RF; BEAM RM.1975; IN: COMPUT. FLUID DYN. CONF. 2. PROC.; HARTFORD, CONN.; 1975; S.L.; AIAA; DA. 1975; PP. 17-28; BIBL. 23 REF.Conference Paper

INSTABILITY OF FINITE DIFFERENCE SCHEMES DUE TO BOUNDARY CONDITIONS IN ELASTIC MEDIA.ILAN A; LOEWENTHAL D.1976; GEOPHYS. PROSPECTG; NETHERL.; DA. 1976; VOL. 24; NO 3; PP. 431-453; BIBL. 13 REF.Article

ELASTIC STRESSES IN TORICONICAL PRESSURE VESSEL HEADS = DEFORMATIONS ELASTIQUES DANS LES EXTREMITES TORICONIQUES D'ENCEINTES SOUS PRESSIONREUSS P.1975; PERIOD. POLYTECH., MED. ENGNG; HONGR.; DA. 1975; VOL. 19; NO 1; PP. 3-10; BIBL. 5REF.Article

UNSTEADY TRANSONIC FLOWS OVER AN AIRFOIL.MAGNUS R; YOSHIHARA H.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1624-1628; BIBL. 8 REF.Article

STABILIZATION OF COWELL'S CLASSICAL FINITE DIFFERENCE METHOD FOR NUMERICAL INTEGRATION. = STABILISATION DE LA METHODE DE DIFFERENCES FINIES CLASSIQUES DE COWELL POUR L'INTEGRATION NUMERIQUEVAN DOOREN R.1974; J. COMPUT. PHYS.; U.S.A.; DA. 1974; VOL. 16; NO 2; PP. 186-192; BIBL. 16 REF.Article

A DISCUSSION OF THE FINITE DIFFERENCE METHOD IN COMPUTER MODELLING OF ELECTRICAL CONDUCTIVITY STRUCTURES. A REPLY TO THE DISCUSSION BY WILLIAMSON, HEWLETT AND TAMMEMAGI.JONES FW; THOMSON DJ.1974; GEOPHYS. J. R. ASTR. SOC.; G.B.; DA. 1974; VOL. 37; NO 3; PP. 537-543; BIBL. 3 REF.Article

ACCURACY OF FINITE-DIFFERENCE MODELING OF THE ACOUSTIC WAVE EQUATION.ALFORD RM; KELLY KR; BOORE DM et al.1974; GEOPHYSICS; U.S.A.; DA. 1974; VOL. 39; NO 6; PP. 834-842; BIBL. 9 REF.Article

A SELF-ADJUSTING GRID FOR FINITE-DIFFERENCE PROGRAMSHURLEY FX; LINBACK RK.1973; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1973; VOL. 5; NO 4; PP. 585-587; BIBL. 8 REF.Serial Issue

ON THE SECOND FUNDAMENTAL PROBLEM OF COMBINED FREE AND FORCED CONVECTION THROUGH VERTICAL NONCIRCULAR DUCTS = SUR LE SECOND PROBLEME FONDAMENTAL DE LA CONVECTION NATURELLE ET DE LA CONVECTION FORCEE A TRAVERS DES CONDUITES VERTICALES NON CIRCULAIRESIQBAL M; KHATRY AK; AGGARWALA BD et al.1972; APPL. SCI. RES.; NETHERL.; DA. 1972; VOL. 26; NO 3-4; PP. 183-208; BIBL. 16 REF.Serial Issue

CONDUCTION THERMIQUE AVEC CONDUCTIBILITE THERMIQUE VARIABLE AVEC LA TEMPERATURE. II. VALIDITE DU FORMALISME VARIATIONNELLORENTSINI EH.1972; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1972; VOL. 23; NO 1; PP. 121-125; ABS. ANGL.; BIBL. 11 REF.Serial Issue

CANCAM 75. 5EME CONGRES CANADIEN DE MECANIQUE APPLIQUEE. COMPTES RENDUS; FREDERICTON, N.B.; 1975.sd; S.L.; DA. S.D.; PP. (819P.); BIBL. DISSEM.Conference Proceedings

MOUVEMENT DANS L'ATMOSPHERE DE CORPS GAZEUX DE FAIBLE DENSITEKUTSAEV AS.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1978; NO 2; PP. 89-93; BIBL. 6 REF.Article

EIN NEUES DIFFERENZENVERFAHREN FUER DIE BEHANDLUNG VON BALKEN UND PLATTEN. I. = NOUVELLE METHODE AUX DIFFERENCES FINIES POUR LE CALCUL DES POUTRES ET DES PLAQUES. INANNI J.1976; Z. ANGEW. MATH. PHYS.; SCHWEIZ.; DA. 1976; VOL. 27; NO 3; PP. 359-369; ABS. ANGL.; BIBL. 5 REF.Article

INTERNAL FLOW CALCULATIONS FOR AXISYMMETRIC SUPERSONIC INLETS AT ANGLE OF ATTACK.PRESLEY LL.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1214; PP. 1-7; BIBL. 11 REF.Conference Paper

APPLICATION DE LA METHODE DES DIFFERENCES FINIES GENERALISEE AU PROBLEME DES PLAQUESTRIBILLO R.1975; ARCH. INZYNIER. LAD.; POLSKA; DA. 1975; VOL. 21; NO 4; PP. 579-586; ABS. RUSSE ANGL.; BIBL. 3 REF.Article

A DIFFERENCE POTENTIAL METHOD FOR INDUCTION SONDES.WHARTON RP.1975; I.E.E.E. TRANS. GEOSCI. ELECTRON.; U.S.A.; DA. 1975; VOL. 13; NO 2; PP. 87-92; BIBL. 7 REF.Article

A FAST SEMIDIRECT METHOD FOR COMPUTING TRANSONIC AERODYNAMIC FLOWS. = METHODE SEMI-DIRECTE RAPIDE POUR CALCULER LES ECOULEMENTS AERODYNAMIQUES TRANSSONIQUESMARTIN ED.1975; IN: COMPUT. FLUID DYN. CONF. 2. PROC.; HARTFORD, CONN.; 1975; S.L.; AIAA; DA. 1975; PP. 162-174; BIBL. 1 P. 1/2Conference Paper

PRACTICAL TECHNIQUES FOR ESTIMATING THE ACCURACY OF FINITE-DIFFERENCE SOLUTIONS TO PARABOLIC EQUATIONSCLAUSING AM.1973; J. APPL. MECH.; U.S.A.; DA. 1973; VOL. 40; NO 1; PP. 61-67; BIBL. 6 REF.Serial Issue

IMPROVED HIGHER-ORDER PANEL METHOD FOR LINEARIZED SUPERSONIC FLOWEHLERS FE; EPTON MA; JOHNSON FT et al.1979; A.I.A.A. J., NEW YORK; USA; DA. 1979; VOL. 17; NO 3; PP. 225-226; BIBL. 4 REF.Article

A COLLOCATION FORMULATION FO WAVE EQUATION MIGRATIONPANN K; SHIN Y; EISNER E et al.1979; GEOPHYSICS; USA; DA. 1979; VOL. 44; NO 4; PP. 712-721; BIBL. 17 REF.Article

COMPUTATION OF THE UNSTEADY FLOW IN AXIAL FLOW COMPRESSORS.PANDOLFI M.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 841; PP. 1-7; BIBL. 8 REF.Conference Paper

IMPLICIT NUMERICAL MODELING OF UNSTEADY FLOWS.AMEIN M; HSIAO LING CHU.1975; PROC. AMER. SOC. CIV. ENGRS, J. HYDRAUL. DIV.; U.S.A.; DA. 1975; VOL. 101; NO 6; PP. 717-731; BIBL. 16 REF.Article

ITERATIVE SOLUTION OF TRANSONIC FLOWS OVER AIRFOILS AND WINGS, INCLUDING FLOWS AT MACH 1.JAMESON A.1974; COMMUNIC. PURE APPL. MATH.; U.S.A.; DA. 1974; VOL. 27; NO 3; PP. 283-309; BIBL. 20 REF.Article

PREDICTIONS IN ENVIRONMENTAL HYDRODYNAMICS USING THE FINITE ELEMENT METHOD.BAKER AJ; ZELAZNY SW.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 7; PP. 1-12; BIBL. 27 REF.Conference Paper

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