Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("FLUIDE NON VISQUEUX")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 3699

  • Page / 148

Export

Selection :

  • and

A PSEUDO THREE-DIMENSIONAL ANALYSIS OF FLOWS IN VANELESS DIFFUSERS FOR MIXED-FLOW COMPRESSORS.WALLACE FJ; ATKEY R; WHITFIELD A et al.1975; J. MECH. ENGNG SCI.; G.B.; DA. 1975; VOL. 17; NO 6; PP. 348-356; BIBL. 19 REF.Article

ECOULEMENT HYPERSONIQUE DE GAZ. ECOULEMENT STATIONNAIRE D'UN GAZ NON VISQUEUX SUR UN CORPSBARANTSEV RG.1976; IN: GIDROMEKH.; MOSKVA; VINITI; DA. 1976; VOL. 9; PP. 5-53; BIBL. 16 P.Book Chapter

SUPERSONIC CASCADE FLOW.LICHTFUSS HJ; STARKEN H.1974; PROGR. AEROSPACE SCI.; G.B.; DA. 1974; VOL. 15; PP. 37-149; ABS. ALLEM. FR.; BIBL. 4 P. 1/2Article

STRUCTURE OF A LINEAR ARRAY OF HOLLOW VORTICES OF FINITE CROSS-SECTION.BAKER GR; SAFFMAN PG; SHEFFIELD JS et al.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 74; NO 3; PP. 469-476; BIBL. 6 REF.Article

AN EXTENSION OF ONE-DIMENSIONAL THEORY TO INVISCID SWIRLING FLOW THROUGH CHOKED NOZZLES.CARPENTER PW; JOHANNESEN NH.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 2; PP. 71-87; BIBL. 1 P. 1/2Article

INSTABILITY OF A DAMPED ROTOR PARTIALLY FILLED WITH AN INVISCID LIQUIDHENDRICKS SL.1981; J. APPL. MECH.; ISSN 0021-8936; USA; DA. 1981; VOL. 48; NO 3; PP. 674-676; BIBL. 5 REF.Article

CALCUL DE L'ECOULEMENT GAZEUX DANS UNE GRILLE DROITE DE PROFILS QUELCONQUESZAJTSEV VP.1978; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; SUN; DA. 1978; NO 3; PP. 112-117; BIBL. 13 REF.Article

ETUDE DES DIFFUSEURS RADIAUX AVEC ECOULEMENT TOURBILLONNAIREVOLOV VT; SHAKHOV VG.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1978; VOL. 21; NO 3; PP. 148-150; BIBL. 3 REF.Article

AERODYNAMICS OF A FINITE ASPECT RATIO JET FLAP AT LOW FLIGHT SPEEDS.ADDESSIO FL; SKIFSTAD JG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 936-943; BIBL. 16 REF.Article

INVISCID ANALYSIS OF TRANSONIC, SLATTEDAIRFOILS.CAUGHEY DA.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 29-35; BIBL. 14 REF.Article

GRUNDLAGEN ZUR EINER THEORIE DES RINGFLUEGELS IN AXIALSYMMETRISCHER SCHERSTROEMUNG.WEISSINGER J; OVERLACH B.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 7-8; PP. 413-421; ABS. ANGL. RUSSE; BIBL. 8 REF.Article

ECOULEMENT AXISYMETRIQUE D'UN FLUIDE INCOMPRESSIBLE ENTRE LES PALES DE TURBOMACHINES AXIALESOTTE JJ.1975; ARCH. BUDOWY MASZ.; POLSKA; DA. 1975; VOL. 22; NO 4; PP. 475-488; ABS. RUSSE ANGL.; BIBL. 24 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

ANALYTICAL THEORY OF THREE DIMENSIONAL FLOUR IN CENTRIFUGAL COMPRESSORSBOSMAN C.1982; J. MECH. ENG. SCI.; ISSN 0022-2542; GBR; DA. 1982; VOL. 23; NO 4; PP. 179-191; BIBL. 17 REF.Article

NEW APPROACH TO INVISCID FLOWBOUNDARYLAYER MATCHING. = NOUVELLE APPROCHE DU RACCORDEMENT ENTRE ECOULEMENT NON VISQUEUX ET COUCHE-LIMITEBRUNE GW; RUBBERT PE; NARK TC JR et al.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 936-938; BIBL. 8 REF.Article

POTENTIALS AND FLOWS ASSOCIATED WITH A LINE SEGMENT.RANGER KB.1975; J. ENGNG MATH.; NETHERL.; DA. 1975; VOL. 9; NO 2; PP. 135-144; BIBL. 4 REF.Article

THEORIE NON LINEAIRE NON STATIONNAIRE DE L'AILE MINCE DE FORME EN PLAN ARBITRAIREBELOTSERKOVSKIJ SM; NISHT MI.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 100-108; BIBL. 11 REF.Article

ECOULEMENT TURBULENT ETABLI AXISYMETRIQUE D'UN FLUIDE NON VISQUEUX DANS LES TURBOMACHINES A PLUSIEURS ETAGESSIROTKIN YA A; STEPANOV G YU.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 6; PP. 3-15; BIBL. 20 REF.Article

THE PRESSURE DISTRIBUTION ON THE SURFACE OF AN ELLIPSOID IN INVISCID FLOWBAND E GU; PAYNE PR.1980; AERONAUT. QUART.; GBR; DA. 1980; VOL. 31; NO 1; PP. 70-84; BIBL. 8 REF.Article

NONLINEAR PREDICTION OF AERODYNAMIC LOADS ON LIFTING SURFACES.KANDIL OA; MOOK DT; NAYFEH AH et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 22-28; BIBL. 1 P.Article

BLOCKAGE EFFECTS ON DRAG OF SHARP-EDGED BODIES.RANGA RAJU KG; VIJAYA SINGH.1976; J. INDUSTR. AERODYN.; NETHERL.; DA. 1976; VOL. 1; NO 3; PP. 301-309; BIBL. 9 REF.Article

NONEXISTENCE OF STATIONARY VORTICES BEHIND A TWO-DIMENSIONAL NORMAL PLATE.SMITH JHB; CLARK RW.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 5; PP. 1114-1115; BIBL. 7 REF.Article

ON THE OPTIMUM FINITE-AMPLITUDE MOTION OF A THRUST-PRODUCING PROFILE.SPARENBERG JA; TAKENS F.1975; J. SHIP. RES.; U.S..A; DA. 1975; VOL. 19; NO 2; PP. 93-98Article

THE STABILITY OF A ROTATING FLOW SUBJECTED TO AN AXIAL PULSATION.MANTON MJ.1975; QUART. J. MECH. APPL. MATH.; G.B.; DA. 1975; VOL. 28; NO 1; PP. 91-105; BIBL. 11 REF.Article

FLOATING SHOCK FITTING TECHNIQUE FOR IMBEDDED SHOCKS IN UNSTEADY MULTIDIMENSIONAL FLOWS.MORETTI G.1974; IN: HEAT TRANSFER FLUID MECH. INST. 24TH MEET. PROC.; CORVALLIS, OREG.; 1974; STANFORD, CALIF.; STANFORD UNIV.; DA. 1974; PP. 184-201; BIBL. 4 REF.Conference Paper

  • Page / 148