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Results 1 to 25 of 1767

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EN ANGLAISHALSEY ND.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 188; PP. 1-11; BIBL. 19 REF.Conference Paper

COMMENT ON "POTENTIAL FLOW ANALYSIS OF MULTIELEMENT AIRFOILS USING CONFORMAL MAPPINGLAURA PAA.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 6; PP. 830; BIBL. 13 REF.Article

INTERFERENCE DES GRILLES MOBILES DANS UN ECOULEMENT POTENTIELSAMOJLOVICH GS; NITUSOV VV.1977; PROBL. PROCHN., U.S.S.R.; S.S.S.R.; DA. 1977; NO 6; PP. 99-102; BIBL. 12 REF.Article

AN INVERSE METHOD FOR THE DESIGN OF MULTIELEMENT HIGH-LIFT SYSTEMS.NARRAMORE JC; BEATTY TD.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 879; PP. 1-7; BIBL. 6 REF.Conference Paper

POTENTIEL DES VITESSES CREEES PAR UNE DISTRIBUTION LOCALISEE DE TOURBILLONSGUIRAUD JP.1978; RECH. AEROSPAT.; FRA; DA. 1978; NO 6; PP. 365-366; ABS. ENG; BIBL. 3 REF.Article

INTERACTION HYDRODYNAMIQUE SUR UN CONTOUR, DU COTE DU COURANT, D'UN FLUIDE INCOMPRESSIBLE IDEAL DE TURBULENCE CONSTANTEVIL'KHOVCHENKO SD.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1978; NO 1; PP. 52-58; BIBL. 11 REF.Article

POTENTIAL FLOW ABOUT IMPULSIVELY STARTED ROTORS.SUMMA JM.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 4; PP. 317-319; BIBL. 4 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

THE USE OF HIGHER-ORDER SURFACE SINGULARITY DISTRIBUTIONS TO OBTAIN IMPROVED POTENTIAL FLOW SOLUTIONS FOR TWO-DIMENSIONAL LIFTING AIRFOILS.HESS JL.1975; COMPUTER METHODS APPL. MECH. ENGNG; NETHERL.; DA. 1975; VOL. 5; NO 1; PP. 11-35; BIBL. 7 REF.Article

LE PROBLEME DE L'ECOULEMENT TRANSITOIRE D'UN LIQUIDE INCOMPRESSIBLE DANS LES ZONES DE CHANGEMENT DE REGIMEEMTSEV BT.1975; TRUDY MOSKOV. ENERGET. INST.; S.S.S.R.; DA. 1975; NO 266; PP. 5-11Article

DAS TEMPERATURFELD EINES GEHEIZTEN ZYLINDERS IN EINER POTENTIALSTROEMUNG. = LE CHAMP DE TEMPERATURE D'UN CYLINDRE CHAUFFE DANS UN ECOULEMENT POTENTIELHERBECK M.1974; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1974; VOL. 54; NO 4; PP. 122-123; BIBL. 3 REF.; (WISS. JAHRESTAG. GES. ANGEW. MATH. MECH. VORTR.; MUENCHEN; 1973)Conference Paper

SINGULARITY-DISTRIBUTIONS FOR CALCULATING PLAN POTENTIAL FLOW AND THREE-DIMENSIONAL ROTATIONALLY SYMMETRIC POTENTIAL FLOW.HOELLER HK.1974; ESCHER WYSS NEWS; SWITZ; DA. 1974; VOL. 47; NO 1; PP. 32-39; BIBL. 6 REF.Article

A NEW APPROACH IN CASCADE FLOW ANALYSIS USING THE FINITE ELEMENT METHODBASKHARONE E; HAMED A.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 1; PP. 65-71; BIBL. 18 REF.Article

POTENTIAL AND VISCOUS FLOW IN STOL OR CTOL PROPULSION SYSTEM INLETS.STOCKMAN NO.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1186; PP. 1-11; BIBL. 17 REF.Conference Paper

VORTEX FORMATION NEAR THE INTAKES TO TURBOMACHINERY AND DUCT SYSTEMS.SWAINSTON MJC.1974; INST. MECH. ENGRS, PROC.; G.B.; DA. 1974; VOL. 188; NO 48; PP. 597-605; BIBL. 11 REF.Article

NAEHERUNGSVERFAHREN ZUR BERECHNUNG DER KOMPRESSIBLEN POTENTIALSTROEMUNG IN EBENEN SCHAUFELGITTERN. = METHODE APPROCHEE POUR CALCULER L'ECOULEMENT POTENTIEL COMPRESSIBLE DANS LES GRILLES D'AUBES BIDIMENSIONNELLESGELLER W.1974; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 68; PP. 1-56; ABS. ANGL.; BIBL. 2 P.Article

COMPUTATIONAL MODEL FOR LOW-SPEED FLOWS PAST AIRFOILS WITH SPOILERSPFEIFFER NJ; ZUMWALT GW.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 3; PP. 376-382; BIBL. 20 REF.Article

THE EXACT AND EXPLICIT SOLUTION TO THE PROBLEM OF THE PLANE POTENTIAL MOTION PAST AEROFOILS OF CARAFOLI TYPEPOPA O.1981; REV. ROUM. SCI. TECH., SER. MEC. APPL.; ISSN 0035-4074; ROM; DA. 1981; VOL. 26; NO 5; PP. 645-658; BIBL. 12 REF.Article

AN IMPROVED IN THE TREATMENT OF SEPARATION IN GENERAL CASCADES BY POTENTIAL FLOW METHODSKADHIM SJ; RAILLY JW.1980; PROC.-INST. MECH. ENG.; ISSN 0020-3483; GBR; DA. 1980-09; VOL. 194; PP. 195-201; BIBL. 6 REF.Article

THE EFFECT OF PERIODIC ERRORS IN BLADE SETTING OF THE POTENTIAL INCOMPRESSIBLE FLOW IN COMPRESSOR CASCADES.EL TAHER MMM; SHAALAN MRA; RASHED MI et al.1978; J. FLUIDS ENGNG; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 22-30; BIBL. 6 REF.Article

A POTENTIAL FLOW DESIGN METHOD FOR MULTICOMPONENT AIRFOIL SECTIONS.KENNEDY JL; MARSDEN DJ.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 1; PP. 47-52; BIBL. 8 REF.Article

THE DEVELOPMENT OF THEORETICAL MODELS FOR JET-INDUCED EFFECTS ON V/STOL AIRCRAFT.SICLARI MJ; MIGDAL D; PALCZA JL et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1216; PP. 1-10; BIBL. 12 REF.Conference Paper

ECOULEMENT POTENTIEL D'UN FLUIDE INCOMPRESSIBLE ENTRE DEUX CONES COAXIAUX SECANTSHLINKA M.1975; STROJN. CAS.; CESKOSL.; DA. 1975; VOL. 26; NO 1; PP. 90-101; ABS. RUSSE; BIBL. 6 REF.Article

AFFAISSEMENT D'UNE CAVITE UNIDIMENSIONNELLEBAUTIN SP.1982; PRIKL. MAT. MEH.; ISSN 0032-8235; SUN; DA. 1982; VOL. 46; NO 1; PP. 50-59; BIBL. 5 REF.Article

METHODE DE CALCUL DE L'ECOULEMENT POTENTIEL SUR UN SYSTEME DE PROFILS AERODYNAMIQUES DANS UN FLUIDE INCOMPRESSIBLEZAJTSEV AA; KOMAROV AM.1979; VEST. MOSKOV. UNIV., 1; SUN; DA. 1979; NO 3; PP. 65-69; ABS. ENG; BIBL. 7 REF.Article

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