Dissymmetry of lift in helicopters

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  • Опубликовано: 14 янв 2025

Комментарии • 6

  • @curtscarlett2475
    @curtscarlett2475 Год назад +3

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

  • @SkyBaum
    @SkyBaum Год назад +3

    Hopefully I'm able to regurgitate this today 🙂

  • @emilianoramirez5398
    @emilianoramirez5398 Месяц назад

    Thank You

  • @diegoplata5570
    @diegoplata5570 Год назад +2

    thanks

  • @stephen5147
    @stephen5147 Год назад +2

    good discussion

  • @hafizuddinmohdlowhim8426
    @hafizuddinmohdlowhim8426 29 дней назад

    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.