Influence of Airfoil Trailing-edge Angle and Trailing-edge Thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers

Influence of Airfoil Trailing-edge Angle and Trailing-edge Thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers PDF Author: Albert D. Hemenover
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Category : Aerofoils
Languages : en
Pages : 764

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The effects of variation of trailing-edge angle and trailing-edge thickness on the lift characteristics of a 10-percent-chord thick symmetrical NACA airfoil section with a 25-percent-chord plain flap are appraised from wind-tunnel tests at Mach numbers from 0.3 to 0.9 and Reynolds numbers varying correspondingly from 1 to 2 million. The airfoil trailing-edge angle was varied from approximately 18 to 6 degrees, and the trailing-edge thickness from zero to the thickness at the flap hinge line.

Influence of Airfoil Trailing-edge Angle and Trailing-edge Thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers

Influence of Airfoil Trailing-edge Angle and Trailing-edge Thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers PDF Author: Albert D. Hemenover
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 764

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Book Description
The effects of variation of trailing-edge angle and trailing-edge thickness on the lift characteristics of a 10-percent-chord thick symmetrical NACA airfoil section with a 25-percent-chord plain flap are appraised from wind-tunnel tests at Mach numbers from 0.3 to 0.9 and Reynolds numbers varying correspondingly from 1 to 2 million. The airfoil trailing-edge angle was varied from approximately 18 to 6 degrees, and the trailing-edge thickness from zero to the thickness at the flap hinge line.

Influence of Airfoil Trailing-edge Angle and Trailing-edge-thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers

Influence of Airfoil Trailing-edge Angle and Trailing-edge-thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers PDF Author: Albert D. Hemenover
Publisher:
ISBN:
Category :
Languages : en
Pages : 103

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 750

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 306

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Subject Index to Unclassified ASTIA Documents

Subject Index to Unclassified ASTIA Documents PDF Author: Defense Documentation Center (U.S.)
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Category : Industrial arts
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Pages : 906

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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
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Category : Aeronautics
Languages : en
Pages : 1308

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Report PDF Author:
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Category : Aeronautics
Languages : en
Pages : 620

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Annual Report PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 534

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 988

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

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Category : Aeronautics
Languages : en
Pages : 1366

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