Search results

Results 1 – 10 of 10
Advanced search

Search in namespaces:

There is a page named "Talk:Pitot theorem" on Wikipedia

  • The text to the lower figure says that the perimeter is P and then that P=|AB|+|CD| which is wrong, because P=|AB|+|BC|+|CD|+|DA|. Episcophagus (talk)...
    2 KB (213 words) - 22:15, 7 February 2024
  • {(-a+b+c+d)(a-b+c+d)(a-b+c-d)(a-b-c+d)}}} and simplified it using Pitot's theorem. The problem is that the sides in a trapezoid are in consecutive order:...
    5 KB (828 words) - 15:06, 27 February 2024
  • long been known that a pitot tube oriented orthogonal to a fluid's motion will measure the static pressure at that point. No. A pitot tube orthogonal to a...
    50 KB (8,120 words) - 17:36, 2 February 2024
  • little more clear. What about Bernoulli's Theorem in discrete mathematics? I think that either Bernoulli's Theorem should not be redirected to here or that...
    125 KB (20,411 words) - 07:52, 21 May 2022
  • that may use either radar altimeters or conventional air data systems with Pitot tubes, there's also the issue of which standards apply when landing at airports...
    14 KB (2,058 words) - 13:16, 1 February 2024
  • consequently changes in static pressure, in accordance with Bernoulli’s Theorem. The distribution of pressure determines the lift, pitching moment and...
    83 KB (12,901 words) - 17:21, 21 June 2017
  • because the hole is on a surface parallel to the flow, as opposed to the Pitot tube, which creates a stagnation point. If somebody still wanted to somehow...
    34 KB (5,577 words) - 22:43, 9 June 2014
  • directly because that's not a real pressure and exerts no real force - a pitot tube wouldn't work if this were true). Dynamic pressure can be converted...
    106 KB (16,879 words) - 04:05, 20 May 2022
  • to construct a wing (or to calculate the airspeed by the pressure using pitot tube).109.174.113.177 (talk) 06:15, 14 July 2021 (UTC)Serg Serg, yes I read...
    48 KB (7,251 words) - 05:06, 11 March 2022
  • (Cessna) and adjacent diagram from here: airplane_wings.htm. A series of pitot static tubes were mounted on a pole about 1/2 foot in front of the wing...
    123 KB (19,319 words) - 02:43, 7 July 2017