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Results 1 to 25 of 126

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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

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

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

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

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

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

INCOMPRESSIBLE SYMMETRIC FLOW CHARACTERISTICS OF SHARP-EDGED RECTANGULAR WINGSLARSON ES.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 6; PP. 508-510; BIBL. 8 REF.Article

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

EXPERIMENTELLE UNTERSUCHUNGEN ZUR ABGELOESTEN STROEMUNG AN EINEM RECHTECKFLUEGEL = ETUDE EXPERIMENTALE DE L'ECOULEMENT DECOLLE SUR UNE AILE RECTANGULAIREBIPPES H; TURK M; JACOB K et al.1981; FORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT-RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1981; NO 12; PP. 1-55; ABS. ENG; BIBL. 12 REF.Serial Issue

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

ETUDE DE LA FORMATION D'UN DECOLLEMENT LAMINAIRE INDUIT PAR LE BRAQUAGE D'UNE GOUVERNESCIBILIA MF; DUROX D.1979; CENTRE NATION. RECH. SCI., LAB. AEROTHERM., RAPP.; FRA; DA. 1979; VOL. 79; NO 2; 9 P.; H.T. 4; BIBL. 7 REF.Serial Issue

CALCUL NUMERIQUE D'ECOULEMENTS TRIDIMENSIONNELS INSTATIONNAIRES AVEC NAPPES TOURBILLONNAIRES.REHBACH C.1977; RECH. AEROSPAT.; FR.; DA. 1977; NO 5; PP. 289-298; ABS. ANGL.; BIBL. 18 REF.Article

ETUDE DE LA FORMATION DU DECOLLEMENT LAMINAIRE INDUIT PAR LE BRAQUAGE D'UNE GOUVERNE EN ECOULEMENT HYPERSONIQUE RAREFIEDUROX D; SCIBILIA MF.1980; AERONAUT. ET ASTRONAUT.; FRA; DA. 1980; NO 81; PP. 21-24; BIBL. 4 REF.Article

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

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

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

Improved Iteration Algorithm for Nonlinear Vortex Lattice MethodLEE, Taeseung; PARK, Seung O.Journal of aircraft. 2009, Vol 46, Num 6, pp 2174-2176, issn 0021-8669, 3 p.Article

Movable tip strakes and wing aerodynamicsNIKOLIC, Vojin R.Journal of aircraft. 2005, Vol 42, Num 6, pp 1418-1426, issn 0021-8669, 9 p.Article

An experimental study of dynamic stall on a finite wingCOTON, F. N; GALBRAITH, R. A. M.Aeronautical Journal. 1999, Vol 103, Num 1023, pp 229-236, issn 0001-9240Article

Flutter prediction for composite wings using parametric studiesGEORGHIADES, G. A; BANERJEE, J. R.AIAA journal. 1997, Vol 35, Num 4, pp 746-748, issn 0001-1452Conference Paper

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