Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Various Stall Control Devices

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Various Stall Control Devices PDF Author: James A. Weiberg
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 54

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Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Various Stall Control Devices

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ratio 5.5, and with Various Stall Control Devices PDF Author: James A. Weiberg
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 54

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Book Description


Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps PDF Author: James A. Weiberg
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

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Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept. Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept. Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps PDF Author: James A. Weiberg
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust

Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust PDF Author: Wallace H. Deckert
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46

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Book Description
Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flap

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flap PDF Author: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C.
Publisher:
ISBN:
Category :
Languages : en
Pages : 1

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Book Description
Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowingtype BLC trailing-edge flaps. The model was tested with flap deflections of 0 degrees without BLC, 50 degrees with and without BLC, and 80 degrees with BLC for wing-tilt angles of 0, 30, and 50 degrees. Included are results of tests of the model equipped with a leading-edge flap and the results of tests of the model in the presence of a ground plane. (Author).

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps PDF Author: James A. Weiberg
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps PDF Author: Roy N. Griffin
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978

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Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References]

Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References] PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47

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Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Area-suction Flaps

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Area-suction Flaps PDF Author: James A. Weiberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76

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Book Description
Comparisons with the results of tests on the same model but having a combination slot suction and blowing boundary-layer-control system (Arado) on the trailing-edge flaps and ailerons indicated considerably lower suction flow requirements for the area-suction flaps.