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ECOULEMENTS A DECOLLEMENT SUR UNE AILE CONIQUE CONCAVEKRAVETS VV; SHVETS AI.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 83-91; BIBL. 12 REF.Article

CALCULATION OF VORTEX BREAKDOWN LOCATIONS FOR FLOW OVER DELTA WINGS.WILSON JD.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 1020-1022; BIBL. 13 REF.Article

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

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

CARACTERISTIQUES AERODYNAMIQUES D'AILES DELTA A VITESSE SUBSONIQUEVORONIN VI.1983; VESTNIK MOSKOVSKOGO UNIVERSITETA. SERIJA 1: MATEMATIKA, MEHANIKA; ISSN 0579-9368; SUN; DA. 1983; NO 1; PP. 89-91; ABS. ENG; BIBL. 4 REF.Article

AERODYNAMIC HEAT TRANSFER TO A HYPERSONIC RESEARCH AIRCRAFT MODEL (X-24C) AT MACH 6.LAWING PL; HUNT JL.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 1018-1020; BIBL. 5 REF.Article

MODERN CONCEPTS FOR DESIGN OF DELTA WINGS FOR SUPERSONIC AIRCRAFT OF SECOND GENERATIONNASTASE A.1979; Z. ANGEW. MATH. MECH.; DDR; DA. 1979; VOL. 59; NO 5; PP. T246-T248; BIBL. 8 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

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

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

MESSUNG UND SICHTBARMACHUNG DER LEESEITIGEN WANDSCHUBSPANNUNGEN BEI DELTAFLUEGELN IM UEBERSCHALL = MESURE ET VISUALISATION DU FROTTEMENT SUPERFICIEL SUR LA FACE SOUS LE VENT D'AILES DELTA EN ECOULEMENT SUPERSONIQUESZODRUCH J; MONSON DJ.1982; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1982; VOL. 6; NO 4; PP. 279-283; ABS. ENG; BIBL. 10 REF.Article

ECOULEMENT STATIONNAIRE SUR LA SURFACE INFERIEURE D'UNE AILE DELTA LOCALEMENT PLANE A ARETES ANTERIEURES SUPERSONIQUESTER MINASYANTS SM.1979; IZV. AKAD. NAUK S.S.S.R., MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1979; NO 5; PP. 80-90; BIBL. 18 REF.Article

PRESSURE DISTRIBUTION ON A SIMPLE DELTA WINGWALKDEN F; CAINE P; MORETTI G et al.1982; COMPUT. FLUIDS; ISSN 0045-7930; USA; DA. 1982; VOL. 10; NO 4; PP. 295-305; BIBL. 8 REF.Article

THE DELTA WING IN OSCILLATORY GNOTSPATEL MH.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 5; PP. 481-486; BIBL. 22 REF.Article

SYNTHESIS OF THE THICKNESS EFFECT IN THE CASE OF FLOW POST A SLENDER DELTA WING WITH LEADING EDGE VORTICESRAY AK; SHARMA S.1979; ACTA MECH.; AUT; DA. 1979; VOL. 33; NO 1-2; PP. 69-80; ABS. GER; BIBL. 11 REF.Article

LEESEITEN-STROEMUNG BEI SCHLANKEN DELTAFLUEGELN ENDLICHER DICKE. = ECOULEMENT DU COTE "SOUS LE VENT" SUR DES AILES DELTA MINCES D'EPAISSEUR FINIESZODRUCH J.1977; I.L.R.-BER.; DTSCH.; DA. 1977; NO 23; PP. 1-146; ABS. ANGL.; BIBL. 8 P.; ISBN 3798305978Serial Issue

OSCILLATING DELTA WINGS WITH ATTACHED SHOCK WAVES.LIU DD; HUI WH.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 6; PP. 804-812; BIBL. 26 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

EFFECTIVENESS OF LEADING-EDGE VORTEX FLAPS ON 60 AND 75 DEGREE DELTA WINGSMARCHMAN JF III.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 4; PP. 280-286; BIBL. 4 REF.Article

HIGH FREQUENCY SOLUTIONS OF THE DELTA WING EQUATIONSHARGRAVE BA.1978; PROC. R. SOC. EDINBURGH, A; GBR; DA. 1978; VOL. 81; NO 3-4; PP. 299-316; BIBL. 10 REF.Article

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