Technical Note - National Advisory Committee for Aeronautics PDF Download
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1304
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1304
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
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Book Description
Author: John A. Kelly
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 706
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Book Description
A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.
Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1838
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Author: Robert E. Dannenberg
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 678
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Book Description
Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 332
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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