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hbykv
เข้าร่วมเมื่อ 7 มี.ค. 2008
Vortex Generator on Sportcruiser
Vortex Generators on Sportcruiser. Lower stall speed. Shorter take off and landing distance. Better climb. Safer to operate the aircraft.
มุมมอง: 8 474
วีดีโอ
VGs on EXPRESS-CT_7,50Min_14,02,2012
มุมมอง 4.8K12 ปีที่แล้ว
Shorter movie with much more information Vortex Generators installed on Express-CT. Continental IO 360ES1B, 6Zyl. 210HP MTOW 1451kg, Cruise Speed 140kt, VNE 210kt. Testflights with actual TOW 1360kg. Stolspeed reduced by 15kt!!! Much better and safer handling, specially for landing. For a few $ or € you get a very big safety margin. Installed and tested Vortex Generators from Stolspeed More inf...
Vortex Generator auf FK14, Mai 2012
มุมมอง 24K12 ปีที่แล้ว
Vortex Generators on FK14 Le Mans No VGs on the wing: even before reaching stall speed the aircraft is loosing aileron control. VGs installed only on the outer wing, in front of the aileron: the aircraft remains controllable down to stall speed. VGs installed over the whole wing: The stall is abrupt and the aircraft is uncontrollable. WARNING: Do not install VGs over the whole wing !!! Ohne VGs...
Vortex Generators on Express-CT.mov
มุมมอง 418K13 ปีที่แล้ว
Vortex Generators installed on Express-CT. Continental IO 360ES1B, 6Zyl. 210HP MTOW 1451kg, Cruise Speed 140kt, VNE 210kt. Testflights with actual TOW 1360kg. Stolspeed reduced by 15kt!!! Much better and safer handling, specially for landing. For a few $ or € you get a very big safety margin. More information on: www.stolspeed.com
Test Drift HD170 Kamera Part 1 in HD
มุมมอง 1.8K13 ปีที่แล้ว
Erster Testflug mit der Drift HD170 Action Camera. Diesmal in HD 720p Qualität. Kamera bei Günter Neugebauer von Blickvang Schweiz i Turbenthal gekauft. Tel 052 385 47 04. www.blickvang.ch/ Grosse Auswahl und gute Beratung.
Drift HD170 Kamera Part 2
มุมมอง 2.1K13 ปีที่แล้ว
Teil 2 vom Test mit der Drift HD170 Action Filmkamera. Einfach schöööön. Habe meine Kamera bei Günter Neugebauer bei Blickvang (Tel 052 385 47 04) in Turbenthal gekauft. Grosse Auswahl und gute Beratung. Part two from the test with the new Drift HD170 Camera. Great fun!!!!!
Test Drift HD170 Kamera
มุมมอง 3K13 ปีที่แล้ว
Erster Test der DRIFT HD170 Action Video Camera aus dem Flugzeug. Start in Locarno LSZL, Flug über den San Bernardino, Walensee und Landung auf dem Flugplatz Speck Fehraltorf LSZK.
Vortex Generators, installation on Zodiac 601UL, August 2010
มุมมอง 7K14 ปีที่แล้ว
This video shows how to install VGs on the airplane and the unbelievable results in flight characteristics and improvement in safety. It demonstrates how the flight safety can dramatically be improved at very low costs with this simple modification. More informations: www.stolspeed.com/ Dieses Video zeigt wie einfach die Montage von Vortex Generators ist. Es veranschaulicht die dramatischen Ver...
Zenair Zodiac 601HDS Testflight with Vortex Generators
มุมมอง 1.7K16 ปีที่แล้ว
Zenair Zodiac 601HDS Experimental with Vortex Generators installed. Demoflight.
Zenair 601HDS Demoflight with Vortex Generators
มุมมอง 14K16 ปีที่แล้ว
Zenair Zodiac 601HDS. Information how to install Vortex Generators and demoflight.
Zenair Zodiac 601HDS Experimental steep turns
มุมมอง 6K16 ปีที่แล้ว
Zenair Zodiac 601 HDS Experimental. Rotax 912 89hp. Vortex Generators from stolspeed.com installed. Low level steep turns. 5 turns 360° in 75 seconds, no speed or altitude loss, due to installed vortex generators.
Zenair Zodiac 601HDS steep turns at 9000ft over Swissalps
มุมมอง 3.1K16 ปีที่แล้ว
Zenair Zodiac 601HDS Experimental, steep turn at 9000ft over the Swissalps. Rotax 912 engine 80hp. Vortex Generators from stolsped.com installed.
T/O hight alt. airport Samedan, 5700ft. Zenair Zodiac 601HDS
มุมมอง 1.6K16 ปีที่แล้ว
T/O in Samedan LSZS, near St. Moritz. Highest airport in Europe. Elevation 5700ft. Zenair Zodiac 601HDS Experimental. Rotax 912 engine 80hp. 2 persons on board and 4h of fuel.Vortex Generators from stolspeed.com installed witch gives much better climb performance.
Zenair Zodiac 601HDS short app LSZS,Samedan elev 5600ft
มุมมอง 3.5K16 ปีที่แล้ว
Short app. to Samedan LSZS in the Swiss alps, Engadin near St. Moritz, highest airport in Eurpe, Elevation 5600ft. Zenair Zodiac 601HDS, Experimental, Rotax 912 80hp. Vortex generators from stolspeed.com instaled.
Zenair Zodiac 601HDS with Vortex Generators
มุมมอง 6K16 ปีที่แล้ว
Testflight with Vortex Generators from stolspeed.com installed only on the outer part of the wing. Powersetting is idle. Tested in Locarn,LSZL south of the Swissalps with 25kt X-wind and heavy Turbulance. Staal speed with this modification is 45kt. Clean wing, no VGs installed stall at 51kt. Complete wing midified with VGs stall at 40kt with idle power. Max power stall at 35kt.
Zenair Zodiac 601HDS Exper. with Vortex Generators installed
มุมมอง 33K16 ปีที่แล้ว
Zenair Zodiac 601HDS Exper. with Vortex Generators installed
Zenair Zodiac 601HDS with Vortex Generators installed
มุมมอง 16K16 ปีที่แล้ว
Zenair Zodiac 601HDS with Vortex Generators installed
Aerodynamics made visible is always so cool to see. I'm glad this popped up in my recommended.
Please how far back from the leading edge were these VG installed? 5%? 8%???
8% back from the leading edge. Viktor
Thank you. Its seems the general thought is that the VG get placed anywhere from 5% to 8-10%. With the idea that the higher angle of attack at stall, like stol plane those get lower percentage install location. And the less angle of attack slippery planes getting the VG placed a few percentages further back from the leading edge. I am no expert but i do a lot of reading. Just what I read.
Loved this video. Loved seeing the tell trails of the when laminar flow detaches. What sort of black magic are VGs?!
This video is awesome. Great work. Surprised all airplanes don't have these installed.
Great video
Excellent experiment ❤❤❤
Wird hier noch mitgelesen bzw kommentiert? Kann ich mir dir Vortex Teile auch selbst an die Fläche kleben? Ja, mir Jd bewusst das diese an bestimmte Positionen muss, hätte eine FK14 mit Vortex fürs aus messen für meine Maschine. LG
Verrückt, was nicht alles möglich ist.. 😛
Watching in April, 2023 for a class in aerodynamics. Thank you!
Fantastic, Thanks!
What was the actual landing speed?
Who else here after the Nepal plane crash, which is suspected due to the stall.😔
No one mr. lowbrainer! People here are mostly smart and have some own knowledge.
Great video. Does the wing have any washout? I'd expect to see this stall pattern (even without VG's) if it does.
Классно
At 2:34 you can see the more dramatic effect is the lateral movement, not the boundary layer backdraft forcing the strings up from the wing. The vortex generators aren't working as described.
look at timestamps. 2:34 is without vgs. 🙂
@@jonasbaine3538 They let anyone in here.
Fantastic video! Thank you for taking the time and also sharing the video! VG clearly make a significant difference to stall speeds at different configs. The transcript is pretty hilarious though - I don't think the researcher actually says "and takes a sexy" at 12:11 🤣
This is the best video I've seen to date on this topic
I now think I know what I’m going to create and stick on my motorcycle’s fairings today. 😁
Why were they put on the tail? What were the results? Was there a benefit? The Wheeler has issues with tail effectiveness at high AOA and side slip. The speeds quoted could be misleading. You could have attached flow on part of the wing but the airplane could be descending I.e. at 0.9g instead of 1g. So the speeds, if you are using them to determine your operating speeds you should correct them by dividing them by the sq root of the vertical acceleration. This is a requirement for defining reference stall speeds on big airplanes. You can’t really claim a super low stall speed if the machine is falling out of the sky and you can’t arrest the sink.
Very interesting experiment! Seems like the ailerons work well past stall angle of attack of the wing. Reminds me of the zigzag tapes we put on som gliders. Low speed handling and induced drag usually improves, at high speed drag can increase but not by much. But it seems to depend on the airfoil shape. If I remember correctly the chordwise placement of turbulator tapes is also rather is critical.
Do anyone come up with the idea of retractable VGs? They could be retracted during the cruise and stick out during take off and landings.
Whats the advantage to retract them?
My question is what were the level cruise speeds differentials with VG and without VG. Was it a large difference between the two. My research has found that it about a 1 to 2 kts difference in level cruise. As with Aviation, there's always a give and take scenario.
I rather lose a few knots and slight fuel use increase to improve controllability in critical situations.
Looking at installing VG on my upcoming plane and want to ensure that I fully understand the need/safety implications/lower stall speeds/lower takeoff and Landing speeds that VG provides.
i hope one day they will make movable vgs as a standards on all planes like they have flaps
What happens if you get ice on them, as ice tends to form first on anything sticking up.
should be avoiding icing conditions with/without vgs! no hot wing!
I'd like to see this on motorcycle windscreens to see if it can reduce helmet buffering while still using a smaller screen.
Guten Abend Herr Strausak / bei Interesse hätte ich Ihnen den link über 7 video's genau zu diesem Thema zu einer einzelnen Lancair in den USA // MFG
Hallo Dani, sehr gerne. Habe vor kurzem einer Lancair Legacy im Birrfeld das sichere Fliegen beigebracht. Einen Bericht darüber gibt es in der AeroRevue Nr. 2/2021. Grüsse Viktor Strausak
@@hbykv ...und weil ich bei der Arbeit (Medienbranche) die AeroRevue durchgearbeitet hatte, bin ich gestern Nacht auf diesen Artikel bzw. link gestossen + hab geantwortet.... :-) // P.S: links kommen noch (= bin aktuell am Arbeiten)....... = leider kein pensionierter Ex-Swissärlär..... :-)
It helped me study
Amazing Video thanks for sharing
Do they cause more drag at higher speeds? More fuel consumption? How much?
Not measurable
Thanks, awesome video!
These arent pilots. These are scientists with a huge pair of balls.
We added a VG kit to our stock standard 160hp Cessna 172N model a few years back and it changed the whole aeroplane. The first Cessna helicopter! The very low speed handling and very slow speed stall characteristics were there to see in the very first flight. Quite amazing really. I wouldn't want to go back to it's previous life not having VG's knowing now what VG's have done to it. In some configurations it seems almost impossible to stall..the ASI reads as low it can go on the dial. You don't even notice any change in IAS. It's only a 100 knot 172 afterall. So that's Yes Yes Yes Yes for VG's..
Great visuals!!
I would advise caution in doing this on half a wing as your changing the loading characteristics along the length of the airfoil.
All planes need VG, they should be standard.
Absolutely correct
With the outer VGs Ropes on the inside: OMG HELL WE ARE STALLING AHHHH MAYDAY MAYDAY Ropes on the outside: Crazy niggas what they doin over der
I see, that they delay the stall but then when the stall does happen it is quicker and more violent. They would also effect fuel economy at the cruise. There's a reason that small plane manufacturers don't use them and I suspect this is why.Many thanks to the poster for doing this video, well done.
Those vortex generators were supplied by stolspeed.com
Correct
ОХУИТЕЛЬНО!!!! :))) 1. Видео как сохнет краска 2. Как бродит квасное сусло + 3. Как дёргаются ниточки на крыле Лайк!!
With those vortex's you can make the tractor fly. Cheibe guet!
Those poor worms.
52 knots, elevator im Aschlag 😂
Cooli sach! :D Echt spannend das so Visuell chönne z gseh.
Such an instructive video. Thanks for your labor. Well done!
Back when I was a CFI, one day I covered the wing of our trainer aircraft with such yarn strips and flew it all day like that, showing student pilots the visual effect of stalling. They were all delighted to see first-hand something they had only studied in textbooks. ...I take it those VGs are not certified for general aviation aircraft? How does one go about installing them? Will the airplane not be illegal with such a radical aerodynamic modification, however beneficial it might be? Would the airplane need to be re-registered as "experimental"?
0:17 This aircraft is experimental. They just had to update the magical paperwork that allows the plane to fly, I assume with data from the VG manufacturer and the new performance data from test flights. I think you can get them for non-experimental, but the manufacturer has to have done all the magical paperwork.
@@jimstanley_49 Somehow I managed to miss the big "experimental" painted there. ...And "magical paperwork" describes it nicely. Thanks for chiming in. Cheers.
Alguém me explica?
Os geradores de vórtice aumentam a energia da "camada limite" (a fina camada de ar mais próxima à superfície da asa). Ao fazer isso, eles atrasam o descolamento da camada limite e com isso conseguem uma redução da velocidade de estol do avião, como mostrado no vídeo.
@@coriscotupi Muito obrigado ❤❤❤
stall?? no way.
Unreal. 15 knot change.