Dissymmetry of lift in helicopters

แชร์
ฝัง
  • เผยแพร่เมื่อ 6 ก.พ. 2025
  • Find more helicopter content over at flight-first.com/

ความคิดเห็น • 6

  • @curtscarlett2475
    @curtscarlett2475 ปีที่แล้ว +3

    searched for a while to have this concept so succinctly explained, thanks!

  • @emilianoramirez5398
    @emilianoramirez5398 หลายเดือนก่อน

    Thank You

  • @diegoplata5570
    @diegoplata5570 ปีที่แล้ว +2

    thanks

  • @SkyBaum
    @SkyBaum ปีที่แล้ว +3

    Hopefully I'm able to regurgitate this today 🙂

  • @stephen5147
    @stephen5147 ปีที่แล้ว +2

    good discussion

  • @hafizuddinmohdlowhim8426
    @hafizuddinmohdlowhim8426 หลายเดือนก่อน

    Your explanation is too complicated. Although not wrong but it is incorrect.
    To use the phrase speed to explain lift generated at rotor system is incorrect because it is rotational system. The right phrase is RPM.
    The rotor spools at the same RPM but with differential lift. Why? Newton first law. It is intended in that way so that the resultant thrust can rotate the helicopter at its own axis quickly. Either up, left, right, forward, or backward.
    By saying quickly, of course, this rotation motion can be achieved with angular momentum but it has a slower response.