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Two aspects of the use of full-and partial-span Gurney flapsNIKOLIC, Vojin R.Journal of aircraft. 2007, Vol 44, Num 5, pp 1745-1748, issn 0021-8669, 4 p.Article

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CALCUL DES CARACTERISTIQUES AERODYNAMIQUES D'UNE AILE D'ENVERGURE FINIEALGAZIN VA.1976; DINAM. SPLOSHN. SREDY; S.S.S.R.; DA. 1976; VOL. 24; PP. 3-14; BIBL. 8 REF.Article

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A BASIC THREE-DIMENSIONAL WING/JET INTERACTION EXPERIMENT.SHOLLENBERGER CA; KOTANSKY DR.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1219; PP. 1-12; BIBL. 18 REF.Conference Paper

EINFLUSS VON TRENNKEILEN AUF DEN AUFTRIEK UND WIDERSTAND EINES RECHTECKFLUGELS MIT STUMPFER HINTERKANTE. = INFLUENCE DES COINS DE SEPARATION SUR LA PORTANCE ET LA TRAINEE D'UNE AILE RECTANGULAIRE A BORD DE FUITE EMOUSSETANNER M.1974; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1974; VOL. 74; NO 61; PP. 1-50; ABS. ANGL.; BIBL. 6 REF.Article

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Wake integration to predict wing span loading from a numerical simulationMATHIAS, D. L; ROSS, J. C; CUMMINGS, R. M et al.Journal of aircraft. 1995, Vol 32, Num 5, pp 1165-1167, issn 0021-8669Article

Effect of viscosity and modes on transonic aerodynamic and aeroelastic characteristics of wingsGURUSWAMY, G. P; MARSTILLER, J. W; YANG, H. T. Y et al.Journal of aircraft. 1985, Vol 22, Num 9, pp 756-762, issn 0021-8669Article

Aerodynamics life at Reynolds numbers below 7 × 10⁴LAITONE, E. V.AIAA journal. 1996, Vol 34, Num 9, pp 1941-1942, issn 0001-1452Conference Paper

Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wingLOTTATI, I.Journal of aircraft. 1985, Vol 22, Num 11, pp 1001-1007, issn 0021-8669Article

QUELQUES PROBLEMES DE LA METHODE D'ETUDE DE LA CHARGE REPARTIE SUR DES AILES VIBRANTESVOLOGODSKIJ VB; IVANOV VV; LAGUTIN VI et al.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 5; PP. 178-181; BIBL. 4 REF.Article

AUFTRIEBS UND WIDERSTANDSMESSUNGEN AN EINEM RECHTECKFLUEGEL MIT TRENNKEIL IM TOTWASSER IM MACHZAHLBEREICH VON 0,5 BIS 1,2. = MESURES DE PORTANCE ET DE TRAINEE SUR UNE AILE RECTANGULAIRE AVEC COIN DE SEPARATION DANS LA ZONE D'EAU MORTE DANS LE DOMAINE DES NOMBRES DE MACH DE 0,5 A 1,2TANNER M.1974; Z. FLUGWISSENSCH.; DTSCH.; DA. 1974; VOL. 22; NO 12; PP. 416-426; ABS. ANGL. FR.; BIBL. 14 REF.Article

A THEORY FOR RECTANGULAR WINGS WITH SMALL TIP CLEARANCE IN A CHANNELSUGIYAMA Y.1973; AERONAUT. QUART.; G.B.; DA. 1973; VOL. 24; NO 2; PP. 103-119; BIBL. 10 REF.Serial Issue

NUMERICAL LIFTING LIME THEORY APPLIED TO DROOPED LEADING-EDGE WINGS BELOW AND ABOVE STALLANDERSON JD JR; CORDA S; VAN WIE DM et al.1980; J. AIRCR.; ISSN 0021-8669; USA; DA. 1980; VOL. 17; NO 12; PP. 898-904; BIBL. 20 REF.Article

AXIAL FLOW MEASUREMENTS IN TRAILING VORTICES.CIFFONE DL; ORLOFF KL.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1154-1155; BIBL. 12 REF.Article

EMBEDDED FLOW CHARACTERISTICS OF SHARP-EDGED RECTANGULAR WINGSLARSON ES.1983; JOURNAL OF AIRCRAFT; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 3; PP. 193-194; BIBL. 5 REF.Article

FLOWFIELD MODEL FOR A RECTANGULAR PLANFORM WING BEYOND STALLWINKELMANN AE; BARLOW JB.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 1006-1008; BIBL. 8 REF.Article

UNIFIED AERODYNAMIC-ACOUSTIC THEORY FOR A THIN RECTANGULAR WING ENCOUNTERING A GUSTMARTINEZ R; WIDNALL SE.1980; A.I.A.A. J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 6; PP. 636-645; BIBL. 17 REF.Article

AN EXPERIMENTAL STUDY OF UNSTEADY AERODYNAMIC FORCES ON A RECTANGULAR WING OSCILLATING IN PITCH AT MACH NUMBERS FROM 0.38 TO 1.28.KIMURA H; NOMIYAMA A.1977; MEM. FAC. ENGNG, KYUSHU UNIV.; JAP.; DA. 1977; VOL. 37; NO 3; PP. 157-174; BIBL. 20 REF.Article

EXPERIMENTE ZUR ENTWICKLUNG DER FREIEN WIRBEL HINTER EINEM RECHTECKFLUEGEL. = ETUDE EXPERIMENTALE DES TOURBILLONS DE TRAINEE DERRIERE UNE AILE RECTANGULAIREBIPPES H.1977; ACTA MECH.; AUTR.; DA. 1977; VOL. 26; NO 1; PP. 223-245; ABS. ANGL.; BIBL. 28 REF.Article

Etude du décrochage instationnaire tridimensional sur une aile rectangulaire = Unsteady three-dimensional stall on a rectangular wingCOSTES, J. J.La Recherche aérospatiale. 1987, Num 4, pp 55-69, issn 0034-1223Article