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

AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING WITH A TIP CLEARANCE IN A CHANNEL.SUGIYAMA Y.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 4; PP. 541-547; BIBL. 8 REF.Article

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

TRANSONIC FLUTTER ANALYSIS OF A RECTANGULAR WING WITH CONVENTIONAL AIRFOIL SECTIONSEASTEP FE; OLSEN JJ.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 10; PP. 1159-1164; BIBL. 14 REF.Article

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

Optimal scheduling of control surfaces on flexible wings to reduce induced dragKOLONAY, Raymond M; EASTEP, Franklin E.Journal of aircraft. 2006, Vol 43, Num 6, pp 1655-1661, issn 0021-8669, 7 p.Article

General equations of motion for an elastic wing and method of solutionSTARK, V. J. E.AIAA journal. 1984, Vol 22, Num 8, pp 1146-1153, issn 0001-1452Article

Behaviour of a rectangular wing a supersonic flow: dynamic pressure and normal force analysis in the range 1.3-4.0 MachETEROVIC, J. E; BARTUREN, O. M; QUARANTA, H. O et al.Computer methods in applied mechanics and engineering. 1985, Vol 53, Num 1, pp 91-94, issn 0045-7825Article

Modélisation du décrochage instationnaire et tridimensionnel = Unsteady stall modelization in a three dimensional flowCOSTES, C; COSTES, J. J; PETOT, D et al.La Recherche aérospatiale. 1985, Num 4, pp 269-271, issn 0034-1223Article

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

Planform variations and aerodynamic efficiency of movable tip strakesNIKOLIC, Vojin R.Journal of aircraft. 2007, Vol 44, Num 1, pp 340-343, issn 0021-8669, 4 p.Article

Optimal rectangular end platesSTANDINGFORD, D. W. F; TUCK, E. O.Journal of aircraft. 1996, Vol 33, Num 3, pp 623-625, issn 0021-8669Article

Effect of longitudinal riblets on the aerodynamic characteristics of a straight wingKONOVALOV, S. F; LASHKOV, YU. A; MIKHAILOV, V. V et al.Fluid dynamics. 1995, Vol 30, Num 2, pp 183-1187, issn 0015-4628Article

The representation of the pressure coefficient surface on the upper side of wedged rectangular wings in supersonic flowNASTASE, A; JAKOBS, R.Zeitschrift für angewandte Mathematik und Mechanik. 1994, Vol 74, Num 5, pp T470-T473, issn 0044-2267Article

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

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

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

UNTERSUCHUNG DES VON EINEM TRAGFLUEGELMODELL IM WINDKANAL ERZEUTEN WIRBELFELDES MITTELS ULTRASCHALLIMPULSEN = ETUDE DU CHAMP DE TOURBILLONS GENERE PAR UNE MAQUETTE DE PROFIL AERODYNAMIQUE DANS UNE SOUFFLERIE AU MOYEN DE PULSATIONS ULTRASONORESENGLER RH; SCHMIDT DW.1979; MITT. MAX-PLANCK-INST. STROEMUNGSFORSCH. AERODYN. VERSUCHSAMT.; DEU; DA. 1979; NO 69; PP. 1-149; ABS. ENG; BIBL. 12 REF.Serial Issue

DAS GESCHWINDIGKEITSPOTENTIAL FUER DEN HARMONISCH SCHWINGENDEN, RECHTECKIGEN FLUEGEL HALBUNENDLICHER SPANNWEITE IN DER NICHTLINEAREN THEORIE = LE POTENTIEL DES VITESSES POUR LES AILES RECTANGULAIRES D'ENVERGURE SEMI INFINIE, OSCILLANT HARMONIQUEMENT, DANS LA THEORIE NON LINEAIRETURBATU S.1981; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1981; VOL. 61; NO 4; PP. T193-T195; BIBL. 9 REF.Article