I’m so glad i found your channel for a detailed aerodynamic breakdown of these topics for the hobbyist
@StartupChuck17 күн бұрын
Thanks for for these videos. It is a great resource in the small niche of tailless aircraft design that is largely ignored. very excited to see more of your wing design and how it performs.
@陳謹揚-q7e2 ай бұрын
Such a high-quality video. Thanks to Gabe, a message from a Taiwanese student who is also majoring in aerospace engineering
@leaky8Ай бұрын
Gabe, thank you for putting these videos together. I'm not an aerospace engineer but I feel like I learned more in these two videos on aerospace than I did in my entire undergraduate program. Incredible detailed, incredibly in depth, absolutely amazing. Looking forward to future videos! Thank you!
@gabefpvАй бұрын
Appreciate that! Glad you found it helpful!
@RealBMK2 ай бұрын
I haven't taken aero yet but I learned so much from this video.
@matthewallen33752 ай бұрын
Your series is great at explaining the process to go from design tasks through formulas, to virtual models ending with a working test model. I appreciate the depth in this series. I have successfully built a RC Prandlt-D flying wing (no vertical surfaces.) from foam board, as tested and detailed out by Albion Bowers formerly at NASA years ago. I have been trying to simplify the build process so other can easily succesd too, this has been helpful on the quest, thank you.
@TheLinessCompany2 ай бұрын
As someone who had a small Module about flying robotics and fell in love with flying wings, this vid is really awesome! Thanks man. :)
@jamesomega2 ай бұрын
Excellent series! I'm really looking forward to your winglet analysis! I used to make rc wings and have test flown all kinds of weird shapes and angles to dampen adverse yaw but I've never seen the variables and their relationships explained so well. Keep up the great work!
@fishercawkeyАй бұрын
Well-done. There's clearly a hunger for this type of content on KZbin, as indicated by the view counts on this video and your Part 1.
@mostowitz842 ай бұрын
Thank you so much for including the explanation of stability derivatives. Looking forward to the other videos!
@mykolakhrystenko28862 ай бұрын
By far, the best video on KZbin on aerodynamics topic! Thank You for your work! Please continue! Waiting for new detailed series on dynamic stability and winglet design!
@notravstar2 ай бұрын
Great series so far, really enjoying the videos keep making them and you'll blow up
@II_xD_II2 ай бұрын
Subbed for this level of details Keep going mate
@onlygaming81062 ай бұрын
Plz continue the series it is really helpful
@grzegorzkolbrecki83442 ай бұрын
Both parts are top notch content, thank You very much!
@II_xD_II2 ай бұрын
Looking forward for whats to come!
@RafaelSanchez-s3fАй бұрын
amazing content!!!!!!!!!!! thank you so much for sharing your knowledge with us!!!!
@Frank-xd4hw2 ай бұрын
Pretty good video. Will there be another one in these series? Have you considered doing one on box wings?
@gabefpv2 ай бұрын
Yeah I’ll keep the series going
@ay_sher2 ай бұрын
Good stuff, would love to see how you counter adverse yaw, and produce directional control.
@rafaelpadilha45852 ай бұрын
Proverse yaw is achieved by ailerons on the tip of the wing, on the part with negative angle of attack. More lift there means forward thrust in that case. There are videos explaining this.
@ay_sher2 ай бұрын
@@rafaelpadilha4585 I guess you're talking about the Prandtl wing and bell shaped wing loading. I have seen the vidoes. But still, YAW CONTROL is missing.
@jedswift2 ай бұрын
Induced drag decreases, not increases with increasing speed. Di = L^2/(πqb^2) or CDi = CL^2/(πA) with q being dynamic pressure, b the wing span, and A as aspect ratio (b^2/wing area).
@gabefpv2 ай бұрын
Whoops, maybe I accidentally said decreases. Totally meant increases! Good catch
@ilyesouadah72992 ай бұрын
incredible videos! love the detail
@hu51162 ай бұрын
Hi Gabe, another fantastic video! You are a master of this! So quick question, can you recommend a top couple of books to cover this in some approximate way to how you do here? Or stated another way, what do you recommend in books? Also, I’d like to recommend taking a look at the “Klingberg wing MkII” channel. He has done some really interesting analysis of a famous flying wing failure and his most recent videos have isolate a really interesting root cause phenomena related to Reynolds Number that is really a core lesson in the vagaries of aerodynamics that I think really highlight some of the things you say about verification.
@gabefpv2 ай бұрын
Yessir, there are a few books in the video description
@hu51162 ай бұрын
@@gabefpv Oooops, sorry missed that! Anyhow your videos are like Tony the Tiger, GREAT! Thanks and look forward to next ones!
@fikumikАй бұрын
16:46 does increased speed really increase induced drag? As far as i know the ind drag coeff drops with the velocity as the AOA decreases, so can we be certain that drag as a force raise?
@gabefpvАй бұрын
This was an error on my end, Q is in the denominator of the induced drag eq, meaning Di decreases with velocity increases
@fikumikАй бұрын
@gabefpv thanks for clarification, great videos tho:)
@jzerious4523Ай бұрын
What program are you using to simulate the flight characteristics?
@gabefpvАй бұрын
Tools like XFLR5, Star-CCM+, Openfoam/fun3d
@dipesh88362 ай бұрын
Hi, whats the reference area for planes in the drag equation? Generally in cars we use the frontal area but a lot of papers are saying that its the wing area for planes? What is actually the reference area
@gabefpv2 ай бұрын
For drag on bluff bodies like cars or parachutes, frontal area should be used. For drag on streamlined bodies like aircraft, the planform area is used for consistency with the lift equation
@dipesh88362 ай бұрын
What sort of Cd are you aiming for with this wing? I am personally designing a speeding with a Cd of 0.05 and am currently at 0.083 Edit: can you please help me out a bit? I am currently using a mh60 airfoil with no twist, naca 009 winglets and a frontal area of 0.00876m^2
@gabefpv2 ай бұрын
Making a winglet design video soon, but if your winglets aren’t toed in try to use a cambered airfoil to extract more negative drag (resultant winglet lift vector due to spanwise flow is tilted slightly forward)
@dipesh88362 ай бұрын
I had another question, do we use the wing area or the frontal area for evaluating drag? From what i know from the automotive side is that the reference area is the frontal area but a lot of the rc plane guys say that its actually the wing area.
@dzfeverframe67872 ай бұрын
Thank you man ❤
@BatataKato2 ай бұрын
🎉🎉🎉 great video
@timothyjudson9191Ай бұрын
Hey mate, would you consider doing a video that is self contained and focused on using diagrams to show that the principles discussed are obvious? I kinda get the math, but I get a little lost in some of the jargon. Making it very intuitive would be huge!
@gabefpvАй бұрын
Sure thing. Can you elaborate a bit?
@timothyjudson9191Ай бұрын
@@gabefpv Imagine that someone who has never taken calculus is watching. The basic ideas should (I hope lol) be transmissible without knowing exactly how to predict it. Starting with that makes the math make a lot of sense too. (This is kinda how I approached rigid body mechanics: concept ----> math)
@gabefpvАй бұрын
Got it. Maybe after this series I’ll do a side series that’s aimed towards those without engineering or mathematics backgrounds! Thanks for the suggestion
@timothyjudson9191Ай бұрын
@@gabefpv~ I re-watched at normal speed and it was a lot easier to understand lol. Btw, where do you study?
@CptPorkster2 ай бұрын
The fastest glow up since Mr Beast
@pranav57772 ай бұрын
can u mention some books to learn this?
@gabefpv2 ай бұрын
@@pranav5777 check out the description
@pranav57772 ай бұрын
@@gabefpv oh i did see it after writing the comment,sry!
@varshneydevansh2 ай бұрын
subbed
@mohammad_physics2 ай бұрын
How i Contact with you
@gabefpv2 ай бұрын
Gabefpv@gmail.com
@NinaNime-eh7ew2 ай бұрын
Dude plz, maybe can you look into upside down v tails
@gabefpv2 ай бұрын
Sure thing
@nidhinkn59802 ай бұрын
Think three forward and backward .
@KlingbergWingMkII2 ай бұрын
This design will be very, very spin prone due to size, shape, and location of the elevons.
@gabefpv2 ай бұрын
I agree, because i designed the example wing in a couple of minutes. Definitely needs twist and sweep optimization
@shayankumarnag86502 ай бұрын
Hello sir
@gabefpv2 ай бұрын
Hello my friend
@shayankumarnag86502 ай бұрын
@@gabefpv sir would you teach me this course please 🙏🙏🙏
@sashgorokhov2 ай бұрын
This one is too theoretical for me. I wish you dived more into practical side of things that can be applied by hobbyists like me
@gabefpv2 ай бұрын
You can design a plane and have these values in XFLR5 in a matter of minutes. If you know what you are looking for in static and dynamic stability modes, you can cut out a whole lot of trial and error when designing RC planes. The videos on fabrication and flight testing are coming soon, too. Just can’t ignore stability when properly designing.
@gabefpv2 ай бұрын
24:30 is about as practical as you can get before just attempting flight with no stability checks (such as only checking CG location on an RC)
@professionalprocrastinator81032 ай бұрын
I don't agree @sashgorokhov, the theoretical grounds are extremely handy for this one video. I'm saying that as someone who wants to understand more about the stability of flying wings as a flight sim dev. Keep going Gabe, this is a gem
@MattExzy2 ай бұрын
I've always found flying wings to be black magic. Nice to have an understanding of the 'why' vs. just whacking on a flight controller, loading firmware, setting pitch & roll limits, and going full send.
@miguelcanoe6774Ай бұрын
The well is deep. Very deep. The surface of the water in the well is as close as the rain brings it. Dig away the hill