Modeling of longitudinal unsteady aerodynamics of a wingtail combination

Modeling of longitudinal unsteady aerodynamics of a wingtail combination PDF Author:
Publisher: DIANE Publishing
ISBN: 1428996788
Category :
Languages : en
Pages : 29

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Modeling of longitudinal unsteady aerodynamics of a wingtail combination

Modeling of longitudinal unsteady aerodynamics of a wingtail combination PDF Author:
Publisher: DIANE Publishing
ISBN: 1428996788
Category :
Languages : en
Pages : 29

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Modeling of Longitudinal Unsteady Aerodynamics of a Wing-Tail Combination

Modeling of Longitudinal Unsteady Aerodynamics of a Wing-Tail Combination PDF Author: Vladislav Klein
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Modeling of Longitudinal Unsteady Aerodynamics of a Wing-Tail Combination

Modeling of Longitudinal Unsteady Aerodynamics of a Wing-Tail Combination PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723743511
Category : Science
Languages : en
Pages : 34

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Aerodynamic equations for the longitudinal motion of an aircraft with a horizontal tail were developed. In this development emphasis was given on obtaining model structure suitable for model identification from experimental data. The resulting aerodynamic models included unsteady effects in the form of linear indicial functions. These functions represented responses in the lift on the wing and tail alone, and interference between those two lifting surfaces. The effect of the wing on the tail was formulated for two different expressions concerning the downwash angle at the tail. The first expression used the Cowley-Glauert approximation known-as "lag-in-downwash," the second took into account growth of the wing circulation and delay in the development of the lift on the tail. Both approaches were demonstrated in two examples using the geometry of a fighter aircraft and a large transport. It was shown that the differences in the two downwash formulations would increase for an aircraft with long tail arm performing low-speed, rapid maneuvers.Klein, VladislavLangley Research CenterUNSTEADY AERODYNAMICS; AERODYNAMIC CHARACTERISTICS; AERODYNAMIC STABILITY; LONGITUDINAL STABILITY; LIFT; PITCHING MOMENTS; WIND TUNNEL TESTS; BODY-WING AND TAIL CONFIGURATIONS; WINGS; TAIL ASSEMBLIES; DOWNWASH; FIGHTER AIRCRAFT

NASA Langley Scientific and Technical Information Output: 1999

NASA Langley Scientific and Technical Information Output: 1999 PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 182

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448

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Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3 - Parameters Estimated from Flight Data

Modeling of Aircraft Unsteady Aerodynamic Characteristics/Part 3 - Parameters Estimated from Flight Data PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 50

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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296

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