Wind-tunnel Investigation of a Deflected-slipstream Cruise-fan V/STOL Aircraft Wing PDF Download
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Author: William A. Newsom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
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Book Description
Author: William A. Newsom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
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Book Description
Author: Michael D. Falarski
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 60
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Book Description
The longitudinal aerodynamic characteristics of a semispan wing dellected-slipstream configuration with a double-slotted flap and and auxiliary wing were determined. The model was powered by two low-pressure-ratio ducted fans. A comparison of static test results with results obtained from various propeller-driven configurations indicates that the turning effectiveness of fan-powered deflected-slipstream configurations can be correlated with propeller-powered configurations with the same flap-chord to slipstream-diameter ratio. The turning effectiveness of the auxiliary wing was essentially the same as would be produced by a conventional slotted flap system with the same flap-chord to slipstream-diameter ratio. The auxiliary wing reduced the thrust required at low speeds as would be expected due to the increase in lifting surface area.
Author: William A. Newsom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 134
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Author: William A. Newsom
Publisher:
ISBN:
Category : Downwash (Aerodynamics)
Languages : en
Pages : 110
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 92
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Author: V. Robert Page
Publisher:
ISBN:
Category : Propeller-driven aircraft
Languages : en
Pages : 58
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Book Description
Author: Michael D. Falarski
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 446
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Book Description
Author: V. Robert Page
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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Book Description
