The aerodynamic behavior of infinite swept wings: another point of viewROSEN, A; RAND, O.Journal of aircraft. 1985, Vol 22, Num 1, pp 83-85, issn 0021-8669Article

Active suppression aeroelastic instabilities on a forward -swept wingNOLL, T. E; EASTEP, F. E; CALICO, R. A et al.Journal of aircraft. 1984, Vol 21, Num 3, pp 202-208, issn 0021-8669Article

Experimental aeroelastic behavior of unswept and forward-swept cantilever graphite/epoxy wingsLANDSBERGER, B. J; DUGUNDJI, J.Journal of aircraft. 1985, Vol 22, Num 8, pp 679-686, issn 0021-8669Article

SOME EARLY EXPERIMENTS IN THE DEVELOPMENT OF A FLYING PLATFORM FOR AERODYNAMIC TESTINGRAMACHANDRA SM.1979; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROM; DA. 1979; VOL. 24; NO 1; PP. 109-117Article

ANWENDUNG UND VERGLEICH MODALER PERTURBATIONSMETHODEN UND MODALER KORREKTURVERFAHREN AM BEISPIEL EINES PFEILFLUEGELS MIT ZWEI PYLONAUSSENLASTEN. = MODIFICATIONS DE STRUCTURE D'UNE MAQUETTE D'AILE FLECHE A DEUX CHARGES EXTERIEURES AU MOYEN DES METHODES DE PERTURBATIONS MODALES ET DE CORRECTIONS MODALESFREYMANN R.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 21; PP. 1-43; ABS. ANGL.; BIBL. 7 REF.Serial Issue

Doublet strip method for oscillating swept tapered wings in incompressible flowICHIKAWA, A.Journal of aircraft. 1985, Vol 22, Num 11, pp 1008-1012, 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

A note on the pressure drag of a forward-swept-wing-plate junctionARNOTT, A. D; BERNSTEIN, L; PETTY, D. G et al.Aeronautical Journal. 1996, Vol 100, Num 997, pp 281-284, issn 0001-9240Article

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

SUR LE MECANISME DE STABILISATION DES "POINTS DE DESTRUCTION" DU TOURBILLON LORS DE L'AERODYNAMIQUE DE L'AILE A TROIS ANGLES A TRAVERS UN ECOULEMENT DE VITESSE SUBSONIQUE FAIBLETRUNEVA EH A.1976; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1976; NO 2; PP. 106-110; BIBL. 3 REF.Article

LIFTING-SURFACE THEORY OF STRAIGHT CASCADES OF SWEPT BLADES.DE O FALCAO AF.1976; INTERNATION. J. MECH. SCI.; G.B.; DA. 1976; VOL. 18; NO 6; PP. 313-320; BIBL. 17 REF.Article

EXPERIMENTAL AND COMPUTATIONAL STUDY OF TRANSONIC FLOW ABOUT SWEPT WINGSBERTELRUD A; BERGMANN MY; COAKLEY J et al.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 16 P.; BIBL. 12 REF.Conference Paper

A WIND TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF FORWARD SWEPT WINGSWEEKS TM; UHUAD GC; LARGE R et al.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 15 P.Conference Paper

SINGULARITY AT THE TRAILING EDGE OF A SWEPT WINGCLAPWORTHY GJ.1979; A.I.A.A. J., NEW YORK; USA; DA. 1979; VOL. 17; NO 3; PP. 313-315; BIBL. 5 REF.Article

WIND TUNNEL MEASUREMENTS OF ROLLING MOMENT IN A SWEPT-WING VORTEX WAKE.EL RAMLY Z; RAINBIRD WJ; EARL DG et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 962-967; BIBL. 15 REF.Article

INTERACTION AERODYNAMIQUE ENTRE UN CANARD PROCHE ET UNE AILE EN FLECHE EN ECOULEMENT TRANSSONIQUEBROCARD Y; SCHMITT V.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 285; 23 P.; ABS. ENG; BIBL. 15 REF.Conference Paper

EFFECT OF SIMULATED JET ENGINES ON THE FLOWFIELD BEHIND A SWEPT-BACK WING.EL RAMLY Z; RAINBIRD WJ.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 4; PP. 343-349; BIBL. 18 REF.Article

LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 551; PP. 1-10; BIBL. 11 REF.Conference Paper

Nonlinear aerodynamics of a delta wing in combined pitch and rollER-EL, J; SETER, D; WEIHS, D et al.Journal of aircraft. 1989, Vol 26, Num 3, pp 254-259, issn 0021-8669Article

An efficient method for computing unsteady transonic aerodynamics of swept wings with control surfacesLIU, D. D; KAO, Y. F; FUNG, K. Y et al.Journal of aircraft. 1988, Vol 25, Num 1, pp 25-31, issn 0021-8669Article

Comment on conical similarity of shock/boundary-layer interactions generated by swept and unswept wings. ReplyBOGDONOFF, S. M; SHUYI WANG; SETTLES, G. S et al.AIAA journal. 1986, Vol 24, Num 3, pp 540-542, issn 0001-1452Article

Aerodynamics of airfoils with vortex trapped by two spanwise fencesROSSOW, V. J.Journal of aircraft. 1994, Vol 31, Num 1, pp 146-153, issn 0021-8669Article

Vortex-induced bending oscillation of a swept wingERICSSON, L. E.Journal of aircraft. 1987, Vol 24, Num 3, pp 195-202, issn 0021-8669Article

Measurements in the turbulent boundary layer on an infinite swept wingBRADSHAW, P; PONTIKOS, N. S.Journal of Fluid Mechanics. 1985, Vol 159, pp 105-130, issn 0022-1120Article

Limit-cycle oscillations of swept-back trapezoidal wings at low subsonic flowSHOKROLLAHI, Saeed; BAKHTIARI-NEJAD, Firooz.Journal of aircraft. 2004, Vol 41, Num 4, pp 948-953, issn 0021-8669, 6 p.Article