Some Theoretical Low-speed Span Loading Characteristics of Swept Wings in Roll and Sideslip PDF Download
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Author: John D. Bird
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
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Book Description
The 7-point method of Weissinger is used to calculate the span loading in roll, lateral center of pressure, and damping in roll for wings having various aspect ratios, sweep angles, and taper ratios. The applicability of the method to the determination of certain other aerodynamic derivatives is investigated, and corrections for the first-order effects of compressibility are indicated.
Author: John D. Bird
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
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Book Description
The 7-point method of Weissinger is used to calculate the span loading in roll, lateral center of pressure, and damping in roll for wings having various aspect ratios, sweep angles, and taper ratios. The applicability of the method to the determination of certain other aerodynamic derivatives is investigated, and corrections for the first-order effects of compressibility are indicated.
Author: John D. Bird
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
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Book Description
Author: Edward Charles Polhamus
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 86
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Book Description
Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
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Book Description
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
Author: John DeYoung
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 106
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Book Description
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 624
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 88
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1208
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Book Description
