Swept Wings | Simple explanation of a complex topic.

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  • čas přidán 28. 06. 2024
  • A swept wing angles backward from its root rather than sideways and is primarily used to increase the Mach-number capability of fast aircraft. This is a complex topic. If you are an engineer, you may wish for a more in-depth explanation. However, for us pilots, this video provides a simplified explanation. It briefly illustrates the theories behind the design of swept-back wings, their pros and cons, and we hope you will find it useful and interesting.
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    Thanks for watching!
    #flightclub #sweptwings

Komentáře • 34

  • @flightclubonline
    @flightclubonline  Před 11 měsíci +5

    WELCOME BACK everyone!
    ALSO CHECK OUT:
    czcams.com/video/BZ75oa1KoaA/video.html
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    • @ShonMardani
      @ShonMardani Před 7 měsíci

      I discovered that Parasite drag is produced by VERTICAL surfaces and Induced drag is created by HORIZONTAL surfaces, for example when the Flaps are at 0 degrees they produce Max Induced drag and Min Parasite drag, at 90 degrees Min Induced and Max Parasite drag and at 45 degrees in the middle of both.
      Please let me know if you think it is a valid observation. Thanks

  • @Aditya-wg3lp
    @Aditya-wg3lp Před 11 měsíci +45

    False, swept wings look cooler, only reason they exist 😤

  • @Tensho_C
    @Tensho_C Před 8 měsíci +8

    I always had an issue with this span-wise vs chord-wise explanation. The airflow only cares about the cross section of the wing that it is flowing parallel to, so why isn't it explained that by sweeping the wings, the thickness of the airfoil in relation to the chord length is smaller, therefore lowering the coefficient of pressure, and delaying the generation of shockwave?

  • @CarryPotter007
    @CarryPotter007 Před 11 měsíci +6

    I can't believe I subconsciously listen to the voice with higher focus and attention than to my uni's professors

  • @kanaprates1012
    @kanaprates1012 Před 11 měsíci +2

    Very interesting, thank you for the content!

  • @mael6791
    @mael6791 Před 10 měsíci +1

    Best channel ever for my selection

  • @almerindaromeira8352
    @almerindaromeira8352 Před 4 měsíci

    Thank you for explaining *both* concepts. The first one I encountered many times but the second one only in written form.

  • @juandowner9070
    @juandowner9070 Před 22 dny

    Amazing video

  • @enzopedrollo
    @enzopedrollo Před 11 měsíci +2

    Well done 👏🏼

  • @chard6649
    @chard6649 Před 11 měsíci +1

    Wow, so compact

  • @brandonsg1367
    @brandonsg1367 Před 4 měsíci +1

    Why would the airflow just magically make a turn when it touches the wing? I don’t understand why the air would go perpendicular to the wing

  • @bartoszskowronski
    @bartoszskowronski Před 11 měsíci +1

    Best explanation.
    Better will be straight wing with longer and thinner cord but this is hard/impossible to build. and less space for fuel.

    • @makantahi3731
      @makantahi3731 Před 2 měsíci

      in airliners, 90% of fuel capacity is in fuselage

  • @flyguy1637
    @flyguy1637 Před 11 měsíci +3

    Love your short videos! Can you do one on how magnetos work!

    • @flightclubonline
      @flightclubonline  Před 11 měsíci +3

      Thank you! Done: czcams.com/video/P5JWuYvf1Jk/video.html

    • @flyguy1637
      @flyguy1637 Před 11 měsíci

      Can you explain how it works when starting the engine so that the spark is strong enough when cranking the engine!

    • @AyYoSteve
      @AyYoSteve Před 9 měsíci

      ​@flyguy1637 impulse couplers! A few good videos on them

  • @cck1496
    @cck1496 Před 11 měsíci +1

    Excellent explanation. Appreciate.

  • @fdc4810
    @fdc4810 Před 11 měsíci +2

    Why does the free stream "know" the swept wing angles though? If we cut a small strip with very small span from both wings, then they would be almost identical except for the leading edge where the swept wing is slightly slanted. Suppose the cord length is the same for both strips, then I would assume both strip would obtain equal lift ? (assuming simplified aerodynamics without considering tip vortex).

    • @FlyLeah
      @FlyLeah Před 10 měsíci

      The swept wing is also tapered, so the pressure gradient is a decreasing curve from wing root to tip, and the slant contributes to the air having to flow with a sideway component due to the uneven pressure gradient (spanwise flow), which is how the air "knows" I’m assuming

  • @2744ducksdman
    @2744ducksdman Před 9 měsíci

    A related reason is that the apparent velocity seen by the wing is less so the drag is also less.

  • @TuCulpa
    @TuCulpa Před 2 měsíci

    Why the reason sweep back wing makes vertical(Y axial) and directional(Z) stability ?

  • @s7lb384
    @s7lb384 Před 4 měsíci

    Can i ask how do you do these animations?

  • @DrR1pper
    @DrR1pper Před 5 měsíci

    So it's just about decreasing the effective thickness-to-cord ratio the airflow "experiences"?

    • @makantahi3731
      @makantahi3731 Před 2 měsíci

      plus thickness of everything else-total aircraft volume distribution(cross section area per length)

  • @vazduplohov
    @vazduplohov Před 9 měsíci +2

    Does anyone know in which software is this video made?

  • @shazam47
    @shazam47 Před 10 měsíci +1

    First rule of flight clib never about flight club

  • @ChrisZoomER
    @ChrisZoomER Před 8 měsíci +3

    Actually, there’s a bigger reason why fast planes have swept wings. Because there’s spanwise flow at all, this means that some of the air flows alongside instead of all of the air being forced over and under the wing in a chordwise flow. This pushed air out of the way more efficiently similar to sliding down a ramp instead of running into a wall. Angling the wings backwards also pulls the center of drag backwards behind the center of gravity so there’s more force that keeps the plane flying nose first.

  • @damianp5781
    @damianp5781 Před 4 měsíci

    Ah, so thats why variabel swept wing airplanes exist