Data from a Static-thrust Investigation of a Large-scale General Research Vtol-stol Model in Ground Effect PDF Download
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Author: Robert J. Huston
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
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Book Description
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller diameters above the ground. The slipstream of the propellers was deflected by tilting the wing and propellers, by deflections of large-chord trailing-edge flaps, and by combinations of flap deflection and wing tilt. Tests were conducted over a range of propeller disk loadings from 7.41 to 29.70 pounds per square foot. Force data for the complete model and pressure distributions for the wing and flaps behind one propeller were recorded and are presented in tabular form without analysis.
Author: Robert J. Huston
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
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Book Description
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller diameters above the ground. The slipstream of the propellers was deflected by tilting the wing and propellers, by deflections of large-chord trailing-edge flaps, and by combinations of flap deflection and wing tilt. Tests were conducted over a range of propeller disk loadings from 7.41 to 29.70 pounds per square foot. Force data for the complete model and pressure distributions for the wing and flaps behind one propeller were recorded and are presented in tabular form without analysis.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 496
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Book Description
Author: Robert J. Huston
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 78
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Book Description
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller diameters above the ground. The slipstream of the propellers was deflected by tilting the wing and propellers, by deflections of large-chord trailing-edge flaps, and by combinations of flap deflection and wing tilt. Tests were conducted over a range of propeller disk loadings from 7.41 to 29.70 pounds per square foot. Force data for the complete model and pressure distributions for the wing and flaps behind one propeller were recorded and are presented in tabular form without analysis.
Author: Robert J. Pegg
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Author: Robert J. Pegg
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Author: John F. Ward
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 28
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
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Author:
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 138
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
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