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Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels PDF Author: Organisation Du Traité De L'Atlantique Nord. Bruxelles. Agard. Neuilly-sur-Seine. Wind tunnel and model testing panel Conférence 1955, juin. Ottawa
Publisher:
ISBN:
Category :
Languages : en
Pages : 161

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Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels PDF Author: Organisation Du Traité De L'Atlantique Nord. Bruxelles. Agard. Neuilly-sur-Seine. Wind tunnel and model testing panel Conférence 1955, juin. Ottawa
Publisher:
ISBN:
Category :
Languages : en
Pages : 161

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Book Description

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels PDF Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 152

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AGARD : Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels

AGARD : Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels PDF Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages :

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Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels, Ottowa, Canada, June, 1955

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels, Ottowa, Canada, June, 1955 PDF Author: Samuel Albert Schaaf
Publisher:
ISBN:
Category :
Languages : en
Pages : 135

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Papers Presented at the Joint Sessionof the Flight Test Techniques and Wind Tunnel and Model Testing Panels, Ottawa, June, 1955

Papers Presented at the Joint Sessionof the Flight Test Techniques and Wind Tunnel and Model Testing Panels, Ottawa, June, 1955 PDF Author: North Atlantic Treaty Organization Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 468

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1208

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Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels

Papers Presented at the Joint Session of the Flight Test Techniques and Wind Tunnel and Model Testing Panels PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 134

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Book Description

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4 PDF Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 644

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This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or fences on the aerodynamic characteristics of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil sections. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.40 to 0.93 and an angle-of-attack range of about -2 degrees to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations. From overall considerations of stability and performance it appears that with the model of this investigation the 6 degree full-span leading-edge flaps in combination with the chord-extension over the outboard 35 percent of the span, with or without leading-edge camber, would be the most desirable configuration.

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508

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Book Description