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  2. File:Examples of Airfoils.svg - Wikipedia

    en.wikipedia.org/wiki/File:Examples_of_Airfoils.svg

    English: Selected airfoils in nature and various vehicles, with their approximate chord length indicated. Sources for the shapes of the airfoils: Low-speed ULM wing: drawn over own photo of low-cost, low-speed ultralight; Propeller blade: drawn over own photo of a sliced WW2-era bomber propeller

  3. NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/NACA_airfoil

    For example, the NACA 2412 airfoil has a maximum camber of 2% located 40% (0.4 chords) from the leading edge with a maximum thickness of 12% of the chord. The NACA 0015 airfoil is symmetrical, the 00 indicating that it has no camber.

  4. Airfoil - Wikipedia

    en.wikipedia.org/wiki/Airfoil

    For example, an airfoil of the NACA 4-digit series such as the NACA 2415 (to be read as 2 – 4 – 15) describes an airfoil with a camber of 0.02 chord located at 0.40 chord, with 0.15 chord of maximum thickness. Finally, important concepts used to describe the airfoil's behaviour when moving through a fluid are:

  5. File:Airfoil geometry.svg - Wikipedia

    en.wikipedia.org/wiki/File:Airfoil_geometry.svg

    This work has been released into the public domain by its author, F l a n k e r.This applies worldwide. In some countries this may not be legally possible; if so: F l a n k e r grants anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law.

  6. File:NACA 4415 (duct profile).svg - Wikipedia

    en.wikipedia.org/wiki/File:NACA_4415_(duct...

    You are free: to share – to copy, distribute and transmit the work; to remix – to adapt the work; Under the following conditions: attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses ...

  7. Puzzle solutions for Wednesday, Dec. 4, 2024

    www.aol.com/news/puzzle-solutions-wednesday-dec...

    Note: Most subscribers have some, but not all, of the puzzles that correspond to the following set of solutions for their local newspaper. CROSSWORDS

  8. Talk:NACA airfoil - Wikipedia

    en.wikipedia.org/wiki/Talk:NACA_airfoil

    TT: the usual two-digit maximum camber in percent of chord; Accordingly, the given example “77887” is nonsensical. You simply cannot have a an “8” in the middle position: it _must_ be either “0” or “1”. An 87%-of-chord thickness is also highly dubious: _none_ of the canonical NACA profiles (10 5-digit and 87 4-digit) go beyond 25%.

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