Effect of Winglets on a First-generation Jet Transport Wing. 6: Stability Characteristics for a Full-span Model at Subsonic Speeds PDF Download
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Author: Stuart G. Flechner
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
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Author: Stuart G. Flechner
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 62
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Author:
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Category : Aeronautics
Languages : en
Pages : 1390
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Category : Astronautics
Languages : en
Pages : 136
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Author: United States. National Aeronautics and Space Administration
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Category : Aeronautics
Languages : en
Pages : 964
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Author: Robert R. Meyer (Jr.)
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Category : Aerodynamic load
Languages : en
Pages : 64
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"The effect of sideslip on winglet loads and selected wing loads was investigated at high and low subsonic Mach numbers. The investigation was conducted in two separate wind tunnel facilities, using two slightly different 0.035-scale full-span models. Results are presented which indicate that, in general, winglet loads as a result of sideslip are analogous to wing loads caused by angle of attack. The center-of-pressure locations on the winglets are somewhat different than might be expected for an analogous wing. The spanwise center of pressure for a winglet tends to be more inboard than for a wing. The most notable chordwise location is a forward center-of-pressure location on the winglet at high sideslip angles. The noted differences between a winglet and an analogous wing are the result of the influence of the wing on the winglet."--Technical report documentation page.
Author: Stuart G. Flechner
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Category : Jet planes, Military
Languages : en
Pages : 76
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Author:
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Category : Aeronautics
Languages : en
Pages : 26
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Author: Robert R. Jr Meyer
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Category :
Languages : en
Pages : 64
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Author: Stuart G. Fletcher
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Category : Airplanes
Languages : en
Pages : 26
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