Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("PORTANCE")

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

Origin

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

Results 1 to 25 of 2938

  • Page / 118
Export

Selection :

  • and

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

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

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

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

TRANSONIC FLOW OVER AN AEROFOIL WITH SPOILER.KANIA W.1975; ROZPR. INZYN.; POLSKA; DA. 1975; VOL. 23; NO 4; PP. 587-596; ABS. POL. RUSSE; BIBL. 11 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

A CONCEPTUAL STUDY FOR A NEW WINGED SURFACE EFFECT VEHICLE SYSTEM = UNE ETUDE CONCEPTUELLE DE NOUVEAU SYSTEME DE VEHICULE A EFFET DE SURFACE MUNI D'AILESMCMASTERS JH; GREER RR.1974; NAV. ENGRS J.; U.S.A.; DA. 1974; VOL. 86; NO 2; PP. 41-51; BIBL. 10 REF.Article

OPTIMAL LIFT CONTROL BY MIELE'S METHOD FOR THE ATMOSPHERIC ENTRY OF A HYPERSONIC GLIDER. II. ISOPERIMETRIC TYPE PROBLEMSBEINER L.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 5; PP. 1039-1053; BIBL. 2 REF.Serial Issue

A NOTE ON LUFFING IN SOILSIRVINE HM.1979; PROC. R. SOC. LONDON, A; GBR; DA. 1979; VOL. 365; NO 1722; PP. 345-347; BIBL. 3 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES NON STATIONNAIRES DE SYSTEMES PORTEURS TRIDIMENSIONNELSPOPYTALOV SA.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 173-176; BIBL. 8 REF.Article

  • Page / 118