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Results 1 to 25 of 4381

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PORTANCES INSTATIONNAIRES SUR UN CYLINDRE VIBRANT DANS UN ECOULEMENT SUPERCRITIQUE.SZECHENYI E; LOISEAU H.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 1; PP. 45-57; ABS. ANGL.; BIBL. 11 REF.Article

BREVET 2.232.236 (B) (7319348). A 28 MAI 1973. DISPOSITIF D'ETANCHEITE ENTRE UNE PIECE FIXE ET UNE PIECE MOBILEsdPatent

BREVET 2.232.237 (B) (7319349). A 28 MAI 1973. DISPOSITIF D'ETANCHEITE ENTRE DEUX SURFACES EN MOUVEMENT RELATIFsdPatent

QUESTION RELATIVE AU PROFIL OPTIMAL D'UNE AILE DANS UN ECOULEMENT DE FLUIDE INCOMPRESSIBLE PARFAITZUBOV VI.1980; ZH. VYCHISLIT. MAT. MAT. FIZ.; SUN; DA. 1980; VOL. 20; NO 1; PP. 241-245; BIBL. 6 REF.Article

LIFT-GENERATED INSTABILITY OF THE PLANE COUETTE FLOW OF A PARTICLE-FLUID MIXTURE.DREW DA.1975; PHYS. OF FLUIDS; U.S.A.; DA. 1975; VOL. 18; NO 8; PP. 935-938; BIBL. 12 REF.Article

FLOW AROUND WINGS WITH INCLINED LATERAL JETS.CARAFOLI E; NEAMTU M.1976; MECH. RES. COMMUNIC.; G.B.; DA. 1976; VOL. 3; NO 3; PP. 163-168; BIBL. 4 REF.Article

CAVITATING FLOW AROUND A CIRCULAR CYLINDER WITH A RADIAL JET GLAPEWERS WA.1979; NATIONAL ENGINEERING LABORATORY. FLUID MECHANICS SILVER JUBILEE CONFERENCE/1979/GLASGOW; GBR; GLASGOW: NEL; DA. 1979; 7.2; 8 P.; H.T. 15; BIBL. 26 REF.Conference Paper

MECANISME DE FORMATION DE LA FORCE NORMALE POUR UN BATTEMENT D'AILESBELOTSERKOVSKIJ SM; GULYAEV VV; NISHT MI et al.1974; IN: IZBR. PROBL. PRIKL. MEKH.; MOSKVA; VINITI; DA. 1974; PP. 97-102; BIBL. 8 REF.Book Chapter

CORRELATION OF WING-BODY COMBINATION LIFT DATA = CORRELATION DE DONNEES DE PORTANCE DE COMBINAISONS AILE-FUSELAGENICOLAI LM; SANCHEZ F.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 126-128; BIBL. 9 REF.Serial Issue

DETERMINATION DE LA VALEUR DE LA PORTANCE DES DISPOSITIFS A FLOTTEUR AVEC UN MOUVEMENT OSCILLANT DU FLOTTEURVAL'KO AD; OZERSKAYA ZI.1980; MEH. TVERD. TELA; ISSN 0572-3299; SUN; DA. 1980; NO 2; PP. 19-28; BIBL. 6 REF.Article

FLIGHT PERFORMANCE OF A CIRCULATION CONTROLLED STOL AIRCRAFT.LOTH JL; FANUCCI JB; ROBERTS SC et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 3; PP. 169-173; BIBL. 8 REF.Article

LIFT.LAUNDRY WE.1975; QUART. BULL. DIV. MECH. ENGNG NATION. AERONAUT. ESTABL.; CANADA; DA. 1975; NO 2; PP. 1-10; BIBL. 2 REF.Article

AILE A ALLONGEMENT MINIMAL AU-DESSUS D'UN ECRAN NON PLANPUTILIN SI.1977; GIDROMEKHANIKA; S.S.S.R.; DA. 1977; NO 35; PP. 29-35; BIBL. 5 REF.Article

COMPUTATION OF AERODYNAMIC LOADS ON HELICOPTER ROTORBLADES IN FOR WARD FLIGHT, USING THE METHOD OF THE ACCELERATION POTENTIAL.VAN HOLTEN T.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 323-334; BIBL. 2 REF.Book Chapter

OPTIMAL LIFT CONTROL BY MIELE'S METHOD FOR THE ATMOSPHERIC ENTRY OF A HYPERSONIC GLIDER. III. HEAT INPUT PROBLEMSBEINER L.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 6; PP. 1223-1235; BIBL. 3 REF.Serial Issue

A PARTIALLY CAVITATING HYDROFOIL OF FINITE SPANUHLMAN JS.1978; J. FLUIDS ENGNG; USA; DA. 1978; VOL. 100; NO 3; PP. 353-354; BIBL. 4 REF.Article

EVALUATION OF A NEW JET FLAP PROPULSIVE-LIFT SYSTEM.YA TUNG CHIN; AIKEN TN; OATES GS JR et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 605-610; BIBL. 6 REF.Article

THE ROLE OF THE NAE 5X5 FOOT WIND TUNNEL IN THE DEVELOPMENT OF MODERN AIRFOIL SECTION.OHMAN LH.1975; IN: ANGLO-AM. AERONAUT. CONF. 14. TECH. PAP.; LOS ANGELES, CALIF.; 1975; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1975; VOL. 959; PP. 1-15; BIBL. 1 P. 1/2Conference Paper

ZUM AUFTRIEBSPROBLEM VON TRAGFLUEGELN MIT WOELBUNG UND VERWINDUNG BEI UEBERSCHALLSTROEMUNG. = PROBLEME DE PORTANCE DES AILES PORTANTES AVEC CAMBRURE ET GAUCHISSEMENT DANS DES ECOULEMENTS SUPERSONIQUESDAS A.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 10; PP. 1-60; ABS. ANGL.; BIBL. 3 P.Article

A SUMMARY OF EXPERIMENTAL RESEARCH ON PROPULSIVE-LIFT CONCEPTORS IN THE LANGLEY 16-FOOT TRANSONIC TUNNEL.CAPONE FJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1315; PP. 1-11; BIBL. 17 REF.Conference Paper

DOUBLET LATTICE-SOURCE METHOD FOR CALCULATING UNSTEADY LOADS ON CAVITATING HYDROFOILSUNRUH JF; BASS RL II.1974; J. HYDRONAUT.; U.S.A.; DA. 1974; VOL. 8; NO 4; PP. 146-153; BIBL. 13 REF.Article

LIFT CORRECTIONS TO TRANSONIC EQUIVALENCE RULE; EXAMPLES.CHENG HK.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 366-373; BIBL. 22 REF.Article

THE EFFECT OF BUOYANCY ON MIXING AND COMBUSTION IN FREE AND ENCLOSED TURBULENT JET DIFFUSION FLAMES AND PLUVERIZED-COAL FLAMES. = EFFET DE LA PORTANCE SUR LE MELANGE ET LA COMBUSTION DANS DES FLAMMES DE DIFFUSION A JET ENCLOS ET TURBULENTS ET DANS DES FLAMMES A CHARBON PULVERISESUNAVALA DP.1976; J. INST. FUEL; G.B.; DA. 1976; VOL. 49; NO 399; PP. 92-103; BIBL. 23 REF.Article

THEORETICAL STUDY OF LIFT-GENERATED VORTEX WAKES DESIGNED TO AVOID ROLLUP.ROSSOV VJ.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 478-484; BIBL. 24 REF.Article

TRANSONIC EQUIVALENCE RULE: A NONLINEAR PROBLEM INVOLVING LIFT.CHENG HK; HAFEZ MM.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 1; PP. 161-187; BIBL. 1 P. 1/2Article

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