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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

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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

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

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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

VORTEX MEASUREMENTS BEHIND A SWEPT WING TRANSPORT MODEL.ORLOFF KL; CIFFONE DL.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 6; PP. 362-364; BIBL. 8 REF.Article

STREAMWISE DEVELOPMENT OF THE FLOW OVER A DELTA WINGSFORZA PM; SMORTO MJ.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 7; PP. 833-834; BIBL. 7 REF.Article

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

THE DEFORMATION OF A VORTEX SHEET BEHIND A SWEPT BACK WING; COMPARISON OF MESUREMENTS AND CALCULATIONS.LABRUJERE TE; DEVRIES O.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 267-277; BIBL. 11 REF.Conference Paper

DIVERGENCE D'UNE AILE A FLECHE AVANTSEJRANYAN AP.1981; MEH. TVERD. TELA; ISSN 0572-3299; SUN; DA. 1981; NO 5; PP. 133-138; BIBL. 10 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

APPLICATION OF AN ADVANCED COMPUTERIZED STRUCTURAL DESIGN SYSTEM TO AN ARROW-WING SUPERSONIC CRUISE AIRCRAFT.ROBINSON JC; YATES EC JR; TURNER MJ et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1038; PP. 1-9; H.T. 2; BIBL. 19 REF.Conference Paper

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

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