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  2. Template:CFB Team Depth Chart - Wikipedia

    en.wikipedia.org/wiki/Template:CFB_Team_Depth_Chart

    1. From the Blank section (below), copy the template tags and parameters to your article. 2. In the template tags, set the Debug parameter to Yes.This will setup the template to display the correct player positions that are needed depending on the Offensive and Defensive schemes that are chosen (OScheme and DScheme parameters) below:

  3. Tie stall - Wikipedia

    en.wikipedia.org/wiki/Tie_stall

    The stall dimensions depend on the cow size, with pregnant and sick cows needing more space. In the Netherland dimensions of 1,85 meter by 1,25 meter are used. In the USA, 52 inch (1,3208 meter) is most common. The front of the stall should be open, so that the cow can lunge forward when standing up. Different materials can be used for the bedding.

  4. List of rail transport modelling scale standards - Wikipedia

    en.wikipedia.org/wiki/List_of_rail_transport...

    Uses a track gauge of 18.83 mm which represents an exact scaling down of the prototype at 4 mm to 1 ft scale. P4 contains an allowance for the tighter curves found on model railways in the wheel back-to-back and related dimensions. S4 removes this allowance, for a dead-scale representation of all trackwork dimensions.

  5. ANSI/ASME Y14.1 - Wikipedia

    en.wikipedia.org/wiki/ANSI/ASME_Y14.1

    A size chart illustrating the ANSI sizes. In 1992, the American National Standards Institute adopted ANSI/ASME Y14.1 Decimal Inch Drawing Sheet Size and Format, [1] which defined a regular series of paper sizes based upon the de facto standard 8 + 1 ⁄ 2 in × 11 in "letter" size to which it assigned the designation "ANSI A".

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  7. Stall (fluid dynamics) - Wikipedia

    en.wikipedia.org/wiki/Stall_(fluid_dynamics)

    The critical angle of attack is typically about 15°, but it may vary significantly depending on the fluid, foil – including its shape, size, and finish – and Reynolds number. Stalls in fixed-wing aircraft are often experienced as a sudden reduction in lift. It may be caused either by the pilot increasing the wing's angle of attack or by a ...