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Persistance et destruction des structures tourbillonnaires concentrées en particulier au-dessus d'ailes delta: critères angulaires de stabilité aux écoulements = Persistance and destruction of the concentrated vortical structures in particular above the delta wings: angular criterion of the stability of the flowBenkir, Mustapha; Le Ray, Michel.1990, 189 p.Thesis

OPTIMISATION DES STRUCTURES D'AVIONPETIAU C; LECINA G.1982; J. MEC. THEOR. APPL.; ISSN 0750-7240; FRA; DA. 1982; VOL. 1; NO 2; PP. 291-309; ABS. ENG; BIBL. 7 REF.Article

FLOWFIELD IN THE PLANE OF SYMMETRY BELOW A DELTA WING.CRAMER MS; GEORGE AR; SEEBASS AR et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 2; PP. 212-215; BIBL. 2 REF.Article

SUPERSONIC FLOW PAST A SLENDER DELTA WING. AN EXPERIMENTAL INVESTIGATION COVERING THE INCIDENCE RANGE-5^O <OU= ALPHA <OU= 50^O.RICHARDS IC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 2; PP. 143-153; BIBL. 15 REF.Article

ANALYSIS AND DESIGN OF STRAKE-WING CONFIGURATIONSLAMAR JE.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 1; PP. 20-27; BIBL. 15 REF.Article

WEITERE UNTERSUCHUNGEN UEBER DIE WIRBELBILDUNG AN FLUEGELN MIT GEKNICKTEN VORDERKANTEN = NOUVELLES ETUDES SUR LA FORMATION D'UN TOURBILLON SUR UNE AILE A BORD D'ATTAQUE EN LIGNE BRISEEBRENNENSTUHL U; HUMMEL D.1982; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1982; VOL. 6; NO 4; PP. 239-247; ABS. ENG; BIBL. 9 REF.Article

EFFECT OF LEADING-EDGE VORTEX FLAPS ON AERODYNAMIC PERFORMANCE OF DELTA WINGSSUBBA REDDY C.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 9; PP. 796-798; BIBL. 8 REF.Article

AILES DELTA ANTISYMETRIQUES D'ORDRE SUPERIEUR EN REGIME SUPERSONIQUESTAICU S.1981; BUL. INST. POLITECH. "GHEORGHE GHEORGHIN-DEJ" BUCARESTI, MEC.; ROM; DA. 1981; VOL. 43; NO 3; PP. 11-20; ABS. RUM; BIBL. 4 REF.Article

FLOW REGIMES OVER DELTA WINGS AT SUPERSONIC AND HYPERSONIC SPEEDS.SQUIRE LC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 1; PP. 1-14; BIBL. 16 REF.Article

INCREASING THE LIFT: DRAG RATIO OF A FLAT DELTA WINGMATTICK AA; STOLLERY JL.1981; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1981; VOL. 85; NO 848; PP. 379-386; BIBL. 2 REF.Article

CALCUL D'UN ECOULEMENT SUPERSONIQUE NON-VISQUEUX SUR UN CORPS PYRAMIDAL SIMULANT UN APPAREIL VOLANT EN DELTAKOSYKH AP; MINAJLOS AN.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 3; PP. 105-111; BIBL. 21 REF.Article

ZUR SYSTEMATIK DER LEESEITEN-STROMUNG BEI DELTAFLUEGELN = TYPES D'ECOULEMENT DU COTE SOUS LE VENT D'AILES DELTASZODRUCH J.1980; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1980; VOL. 4; NO 2; PP. 72-81; ABS. ENG; BIBL. 19 REF.Article

DELTA WING WITH BLOWING OR SUCTION THROUGH THE SURFACE.CARAFOLI E; POPA R.1975; REV. ROUMAINE SCI.-TECH., MEC. APPL.; ROUMAN.; DA. 1975; VOL. 20; NO 1; PP. 27-40; BIBL. 5 REF.Article

SICHTBARMACHUNG DER UMSTROEMUNG ZWEIER RAUMGLEITERKONFIGURATIONEN IM UNTERSCHALLBEREICH. = VISUALISATION DE L'ECOULEMENT AUTOUR DE DEUX PROFILS DANS LE DOMAINE SUBSONIQUEBIPPES H; COLAK ANTIC P.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 49; PP. 1-45; H.T. 14; ABS. ANGL.; BIBL. 2 P.Serial Issue

VORTEX-LATTICE METHOD FOR THE CALCULATION OF THE NONSTEADY SEPARATED FLOW OVER DELTA WINGSLEVIN D; KATZ J.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 12; PP. 1032-1037; BIBL. 21 REF.Article

ON LIFT OF DELTA WINGS WITH LEADING-EDGE VORTICESHAYASHIDA M; SATO M; MATSUOKA K et al.1977; BULL. UNIV. OSAKA PREFECT., A; JPN; DA. 1977; VOL. 26; NO 2; PP. 37-51; BIBL. 19 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

UNSTEADY AERODYNAMICS OF SLENDER DELTA WINGS AT LARGE ANGLES OF ATTACK.ERICSSON LE; REDING JP.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 9; PP. 721-729; BIBL. 41 REF.Article

A SOLUTION FOR CONICALLY CAMBERED DELTA WINGS IN SUPERSONIC FLOW.MATEESCU D.1975; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1975; VOL. 20; NO 2; PP. 189-216; BIBL. 7 REF.Article

CAREFUL NUMERICAL STUDY OF FLOWFIELDS ABOUT SYMMETRIC EXTERNAL CONICAL CORNERSSALAS MD.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 6; PP. 646-651; BIBL. 15 REF.Article

INVESTIGATION OF LEADING-EDGE DEVICES FOR DRAG REDUCTION OF A 60-DEGREE DELTA WING AT HIGH ANGLES OF ATTACKRAO DM; JOHNSON TD JR.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 10 P.; BIBL. 4 REF.Conference Paper

STREAMWISE DEVELOPMENT OF THE FLOW OVER A DELTA WINGSFORZA PM; SMORTO MJ.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 7 P.; BIBL. 10 REF.Conference Paper

THE CALCULATION OF NON-LINEAR AERODYNAMIC CHARACTERISTICS OF WINGS AND THEIR WAKES IN SUBSONIC FLOWZOREA CR; ROM J.1978; ISRAEL J. TECHNOL.; ISR; DA. 1978; VOL. 16; NO 1-2; PP. 83-96; BIBL. 32 REF.Conference Paper

LOAD DISTRIBUTIONS ON SLENDER DELTA WINGS HAVING VORTEX FLOW.KUHLMAN J.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 699-702; BIBL. 8 REF.Article