Author: P.R. Owen
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Interference Between the Wings and the Tailplane of a Slender Wing-body-tailplane Combination
Author: P.R. Owen
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Interference Between the Wings and the Tail Surfaces of a Combination of Slender Body, Cruciform Wings and Cruciform Tail Set at Both Incidence and Yaw
Author: P.R. Owen
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Aerodynamic Interference of Slender Wing-tail Combinations
Author: Alvin H. Sacks
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 81
Book Description
Mathematical expressions are derived for the interference forces and moments acting on the tails of slender plane and cruciform wing-tail combinations of general plan form in steady straight flight at combined angles of attack and sideslip. The derivatives are made within the limitations of slender-body theory under the assumption that the vortex sheet leaves the wing as flat sheet and becomes fully rolled up ahead of the tail. The derived expressions are used to calculate the steady lifts, side forces, pitching moments, and rolling moments of the number of wing-tail combinations. The effects of changes in tail height, tail length, ratio of tail span to wing span, tail incidence, and tail thickness are calculated. The resulting curves, and particularly their nonlinearities, are discussed at some length in connection with static stability. In general, the most dramatic effects are noted when the vortices shed from the wing strike the tips of the tail trailing edge.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 81
Book Description
Mathematical expressions are derived for the interference forces and moments acting on the tails of slender plane and cruciform wing-tail combinations of general plan form in steady straight flight at combined angles of attack and sideslip. The derivatives are made within the limitations of slender-body theory under the assumption that the vortex sheet leaves the wing as flat sheet and becomes fully rolled up ahead of the tail. The derived expressions are used to calculate the steady lifts, side forces, pitching moments, and rolling moments of the number of wing-tail combinations. The effects of changes in tail height, tail length, ratio of tail span to wing span, tail incidence, and tail thickness are calculated. The resulting curves, and particularly their nonlinearities, are discussed at some length in connection with static stability. In general, the most dramatic effects are noted when the vortices shed from the wing strike the tips of the tail trailing edge.
Current Papers
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 846
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 846
Book Description
Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 922
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 922
Book Description
Journal of the Royal Aeronautical Society
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 976
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 976
Book Description
Technical Report
Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 684
Book Description
Includes its Reports, which are also issued separately.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 684
Book Description
Includes its Reports, which are also issued separately.
Report
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages : 684
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 684
Book Description
The Journal of the Royal Aeronautical Society
Author: Royal Aeronautical Society
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
Book Description
Reports and Memoranda
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1028
Book Description
Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1028
Book Description
Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.