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flèche de l'aile

sweepback

technologie et réglementation technique - iate.europa.eu

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Plaice 4 s 6d netsome flutter tests on swept-back wings ground-launched rocketssweepback....

général - core.ac.uk - PDF: citeseerx.ist.psu.edu

Wind tunnel pressure distribution tests on a series of biplane wing models. part iii effects of charges in various combinations of stagger, gap, sweepback, and decalageThis preliminary report furnishes information on the changes in the forces on each wing of a biplane cellule for various combinations of stagger and gap, stagger and sweepback, stagger and decalage, and gap and decalage....

PDF: hdl.handle.net

Wind tunnel pressure distribution tests on a series of biplane wing models part ii : effects of changes in decalage, dihedral, sweepback and overhangThis preliminary report furnishes information on the changes in the forces on each wing of a biplane cellule when the decalage, dihedral, sweepback and overhang are separately varied....

PDF: hdl.handle.net

Span load distribution on two monoplanes wing models as affected by twist and sweepbackThe results presented in this note show the effect of twist and sweepback on the span load distribution over two monoplane wing models....

PDF: hdl.handle.net

Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 atWind-tunnel studies were conducted to determine the effect of leading-edge sweepback on the lift, drag, and pitching-moment characteristics of 3-percent-thick wings of aspect ratio 3 and taper ratio 0.11.....

PDF: digital.library.unt.edu

wing sweepback

technologie et réglementation technique - iate.europa.eu

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Price £2 0s. 0d. netflight tests on the short sb5 with 60 °... The Short SB 5 is a low-speed research aircraft capable of operation with wing sweepback angles of 50 °, 60 °, or 69 °, various wing leading-edge configurations, and a high or low tailplane....

général - core.ac.uk - PDF: citeseerx.ist.psu.edu

Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at mach 6... The wing sweepback angles are 0, 50, and 70 degrees....

PDF: hdl.handle.net

:os. 6d. netwind-tunnel tests on the effect of a localised mass on the flutter of a swept-back wing with fixed root by... The investigation covers the effects of wing sweepback, and of the magnitude and position of the localised mass....

PDF: citeseerx.ist.psu.edu

A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with naca 64a thickness distributions, fences, a leading-edge extension, and body contouring /An investigation has been made to determine the effect of wing fences, a wing leading-edge extension, changing wing sweepback angle from 40 to 45 and 50 degrees, fuselage contouring, and varying horizontal tail height upon the buffeting response of some typical airplane configurations ...

PDF: www.hathitrust.org

Aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a 1/14-scale model of the grumman xf104 airplane with wing sweepback of 42.5 degreesAn investigation has been made at high subsonic speeds of the aerodynamic'characteristics in pitch and sideslip of a l/l4-scale model of the Grumman XF10F airplane with a wing sweepback angle of 42.5....

PDF: hdl.handle.net