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kw.\*:("DELTA WING")

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Results 1 to 25 of 479

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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

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

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

SPANWISE CAMBERED DELTA WING WITH LEADING-EDGE SEPARATION.FERNANDEZ J; HOLLA VS.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 3; PP. 276-282; BIBL. 14 REF.Article

USE OF HIGH CONICAL FLOW THEORY FOR THE DETERMINATION OF THE PRESSURE DISTRIBUTION ON THE WAVE RIDER AND ITS AGREEMENT WITH EXPERIMENTAL RESULTS FOR SUPERSONIC FLOWNASTASE A; STAHL H.1981; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1981; VOL. 61; NO 4; PP. T165-T168; BIBL. 13 REF.Article

MEASUREMENT OF SHOCK WAVES AROUND A DELTA-WING SEMICONEKIMURA T; NISHIO M.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 7; PP. 843-844; BIBL. 9 REF.Article

AGREEMENT OF HIGH CONICAL FLOW THEORY WITH EXPERIMENTAL RESULTS FOR SUPERSONIC FLOWNASTASE A.1980; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T199-T201; BIBL. 8 REF.Article

GENERALIZED AREA RULES AND INTEGRAL THEOREMS FOR HYPERSONIC WING-BODIESMALMUTH ND.1978; A.I.A.A. J. NEW YORK; USA; DA. 1978; VOL. 16; NO 9; PP. 1019-1022; BIBL. 9 REF.Article

HYPERSONIC FLOW WITH ATTACHED SHOCK WAVES OVER PLANE DELTA WINGS.WOODS BA; MCINTOSH CBG.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 79; NO 2; PP. 361-377; BIBL. 17 REF.Article

NUMERICAL STUDY OF FLOWFIELDS ABOUT ASYMMETRIC EXTERNAL CONICAL CORNERSSALAS MD.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1661-1667; BIBL. 9 REF.Article

ECOULEMENT SUPERSONIQUE ANTI-SYMETRIQUE AUTOUR DE L'AILE DELTA, AVEC DETACHEMENT DU COURANT AUX BORDSSTAICU S.1980; BUL. INST. POLITEH. "GHEORGE GHEORGIU-DEJ" BUCURESTI, MEC.; ROM; DA. 1980; VOL. 42; NO 1; PP. 29-37; ABS. RUM; BIBL. 3 REF.Article

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