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 : 530
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Book Description
Author: Editors of Klutz
Publisher:
ISBN: 9781338643923
Category :
Languages : en
Pages :
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Book Description
Fanciful fairies will love creating their own crowns, wings, and wands. Lush artwork includes flowers, leaves, snowflakes, shells, and starfish to assemble into adjustable fairy crowns. The wings loop easily around little fairies' arms. Make two smaller pixie-sized wands and one deluxe wand by filling the tubes with glitter, and then assembling beads, ribbon, and papercraft into whimsical wand toppers. Crystal-clear instructions show how to assemble each project, so there's no need to wing it. Comes with: Wand, wand cap, fairy dust glitter, ribbon in 4 colors, 69 ponybeads in 2 colors, 2 fairy wings, foam wing center, 2 elastic bands, 3 punch-out sheets, 4 pipe cleaners, 3 iridescent sheets.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 530
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Book Description
Author: Great Britain. Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 958
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 404
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Book Description
Author: Williams J. Alford
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 30
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Book Description
Author:
Publisher:
ISBN:
Category : Book clubs (Discussion groups)
Languages : en
Pages : 556
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Book Description
Author: Frederick C. Grant
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
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Book Description
Author: E. Claude Sanders
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 840
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Book Description
Author: Robert J. Platt
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50
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Book Description
A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-foot transonic pressure tunnel. The tests covered wings with a thickness ratio of 6 percent for sweepback angles of 0, 25, and 45 degrees and a thickness ratio of 4 percent for an unswept wing.
