kw.\*:("NAPPE TOURBILLON")
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ON A GENERALIZATION OF KADEN'S PROBLEMPULLIN DI; PHILLIPS WRC.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 104; PP. 45-53; BIBL. 17 REF.Article
A HIGHER ORDER PANEL METHOD APPLIED TO VORTEX SHEET ROLL-UPHOEIJMAKERS HWM; VAATSTRA W.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 4; PP. 516-523; BIBL. 26 REF.Article
A SEMI-ANALYTIC APPROACH TO THE SELF-INDUCED MOTION OF VORTEX SHEETSSCHWARTZ LW.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981-10; VOL. 111; PP. 475-490; BIBL. 13 REF.Article
ESTIMATION OF VELOCITIES AND ROLL-UP IN AIRCRAFT VORTEX WAKES.BILANIN AJ; DUP DONALDSON C.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 578-585; BIBL. 27 REF.Article
CALCULATION OF INITIAL VORTEX ROLL-UP IN AIRCRAFT WAKES.BERA RK.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 58-59; BIBL. 4 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
COMMENT ON THEORETICAL STUDY OF LIFT-GENERATED VORTEX WAKES DESIGNED TO AVOID ROLLUP.TURGUT SARPKAYA; ROSSOW VJ.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 12; PP. 1680-1682; BIBL. 8 REF.Article
CALCUL NUMERIQUE D'ECOULEMENTS AVEC NAPPES TOURBILLONNAIRES ENROULEESHUBERSON S.1980; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1980; NO 3; PP. 197-203; ABS. ENG; BIBL. 17 REF.Article
ENROULEMENT DE NAPPES DE TOURBILLONS ISSUES DE CONTOURS DE SURFACES PORTANTESLEGENDRE R.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 3; PP. 143-147; ABS. ENG; BIBL. 11 REF.Article
A TEST OF THE METHOD OF FINK & SOH FOR FOLLOWING VORTEX-SHEET MOTIONBAKER GR.1980; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1980; VOL. 100; NO 1; PP. 209-220; BIBL. 17 REF.Article
ANALYTIC STRUCTURE OF VORTEX SHEET DYNAMICS. I: KELVIN-HELMHOLTZ INSTABILITYMEIRON DI; BAKER GR; ORSZAG SA et al.1982; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1982; VOL. 114; PP. 283-298; BIBL. 15 REF.Article
THE INTERACTION OF SOUND WITH A SEMI-INFINITE VORTEX SHEET.MORGAN JD.1974; QUART. J. MECH. APPL. MATH.; G.B.; DA. 1974; VOL. 27; NO 4; PP. 465-487; BIBL. 7 REF.Article
SOME TECHNIQUES FOR EXTENDING THE APPLICATION OF THE DISCRETE VORTEX METHOD OF FLOW SIMULATIONBROMILOW IG; CLEMENTS RR.1982; AERONAUT. Q.; ISSN 0001-9259; GBR; DA. 1982; VOL. 33; PART. 1; PP. 73-89; BIBL. 16 REF.Article
ETUDE PAR VISUALISATIONS HYDRODYNAMIQUES, DE DIVERS PROCEDES DE CONTROLE D'ECOULEMENTS DECOLLES.WERLE H; GALLON M.1976; RECH. AEROSPAT.; FR.; DA. 1976; NO 2; PP. 75-94; ABS. ANGL.; BIBL. 34 REF.Article
THREE-DIMENSIONAL SOLUTION OF FLOWS OVER WINGS WITH LEADING-EDGE VORTEX SEPARATION.WEBER JA; BRUNE GW; JOHNSON FT et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 4; PP. 519-525; BIBL. 13 REF.Article
THE TRANSMISSION OF DEEP-WATER WAVES ACROSS A VORTEX SHEET.EVASN DV.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 68; NO 2; PP. 389-401; BIBL. 14 REF.Article
THE DEFORMATION OF A VORTEX SHEET BEHIND A SWEPT BACK WING; COMPARISON OF MESUREMENTS AND CALCULATIONS.LABRUJERE TE; DEVRIES O.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 267-277; BIBL. 11 REF.Conference Paper
CALCUL DES CARACTERISTIQUES AERODYNAMIQUES NON LINEAIRES D'UNE AILE DE FORME COMPLEXE DANS LE PLAN EN TENANT COMPTE DE LA NAPPE TOURBILLONNAIRE DE L'AVANTAPARINOV VA.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 2; PP. 107-111; BIBL. 4 REF.Article
UNSTEADY MOTION OF AIRFOILS WITH BOUNDARY- LAYER SEPARATION.SEARS WR.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 2; PP. 216-220; BIBL. 9 REF.Article
APPROXIMATION LOCALE D'UNE NAPPE TOURBILLONNAIRE PAR UN SYSTEME DE TOURBILLONS DISCRETSGORELOV DN.1980; P.M.T.F.; SUN; DA. 1980; NO 5; PP. 76-82; BIBL. 9 REF.Article
GLEICHGEWICHT, EFFEKTIVES IMPULSVERHAELTNIS UND STABILITAET VON ENDLICHEN, EINPARAMETRIGEN EBENEN WIRBELSYSTEMEN. = EQUILIBRE, RAPPORT EFFECTIF DES IMPULSIONS ET STABILITE DE SYSTEMES DE TOURBILLONS FINIS, A UN PARAMETRE ET PLANSSTUMKE H.1975; INGR-ARCH.; DTSCH.; DA. 1975; VOL. 44; NO 4; PP. 239-253; ABS. ANGL.; BIBL. 33 REF.Article
A THREE DIMENSIONAL SOLUTION OF FLOWS OVER WINGS WITH LEADING-EEDGE VORTEX SEPARATION.WEBER JA; BRUNE GW; JOHNSON FT et al.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 866; PP. 1-8; BIBL. 13 REF.Conference Paper
RADIATION PROPERTIES OF THE SEMI-INFINITE VORTEX SHEET: THE INITIAL-VALUE PROBLEM.CRIGHTON DG; LEPPINGTON FG.1974; J. FLUID MECH.; G.B.; DA. 1974; VOL. 64; NO 2; PP. 393-414; BIBL. 11 REF.Article
CALCUL D'UNE AILE ELANCEE AVEC NAPPES DE TOURBILLONS S'ENROULANT LE LONG DES BORDS LATERAUXNONAKA K.1974; J. SOC. NAV. ARCHITECTS JAP.; JAP.; DA. 1974; VOL. 135; PP. 63-69; ABS. ANGL.; BIBL. 7 REF.Article
SUBVORTEX TECHNIQUE FOR THE CLOSE APPROACH TO A DISCRETIZED VORTEX SHEET.MASKEW B.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 188-193; BIBL. 8 REF.Article