Noodles
Member
will doLMAO...
Please post a build thread. The planes you are modelling are very modern and will likely draw interest.![]()
will doLMAO...
Please post a build thread. The planes you are modelling are very modern and will likely draw interest.![]()
As far as I know, the Cobra is just a straight forward flare to a very high angle of attack. ...
In aerobatics, Pugachev's Cobra (or Pugachev Cobra) is a dramatic and demanding maneuver in which an airplane flying at a moderate speed suddenly raises the nose momentarily to the vertical position and slightly beyond, before dropping it back to normal flight. It relies on powerful engine thrust to maintain approximately constant altitude through the entire move
Just for completeness, Pugachev's Cobra is a very specific maneuver.
It involves pitching up to beyond 180 degrees AOA and then pitching forward to normal AOA flight.
Wikipedia has a good short description and excellent diagram:
View attachment 144529
By wikipedia user Henrickson, CC BY-SA 3.0, https://commons.wikimedia.org/w/index.php?curid=5469045
Forgive me my ignorance. I am and will forever be a student of this great hobby that is RC flight. I just don't see the difficulty here. Fly forward. Nose up. Drop throttle. Nose down. Increase throttle. There's some obvious elevator work going on in there, but nothing that seems amazing.
Doing so without losing forward speed would take some finesse, but it doesn't seem that far out. What am I missing?
Yeah that's why I said if he's going with props use a 3 or 4 blade. Less efficient, but lots of that spare thrust that helps on maneuvers like that. A thrust vectoring setup, or at least a prop in slot with some good wash over the control surfaces should do the trick. Still not the easiest maneuver to retain stability. I've done some ridiculous high alpha but not past 180 degrees.The part where you stall out, faceplant into the deck and your plane goes home in a bag...
I think you would need to have a lot of thrust available to pull that maneuver off and I think that's what this stunt demonstrates.
I don't think you could pull it off with a model of a B-25. Then again, it could be fun to try.![]()
Ooohhhh. That's a job for...... "Wait! Look! what is that, up there in the sky? Why it's the Super Plane! It's the Mini Scout Biplane! I bet she can do it!"The part where you stall out, faceplant into the deck and your plane goes home in a bag...
I think you would need to have a lot of thrust available to pull that maneuver off and I think that's what this stunt demonstrates.
I don't think you could pull it off with a model of a B-25. Then again, it could be fun to try.![]()
@Mid7night's F-18 and F-16 both cobra just fine. Personally, I think all you need is a swept leading edge (for stability) and a ton of elevator.
... I just don't see the difficulty here. Fly forward. Nose up. Drop throttle. Nose down. Increase throttle. There's some obvious elevator work going on in there, but nothing that seems amazing. ... What am I missing?
I've seen a lot of F-16 and F-18 demonstrations, and I've never seen (or heard) that either plane can do a cobra maneuver.
The only US Air Force plane I know of that can pull it off is the F-22.
The symmetrical air flow thing is a big issue not just with the Cobra, but with all extreme high angle of attack maneuvers in order for the plane to keep its balance. The LERX thing a lot of fighters use is sort of akin to the whole wing itself on my little slender delta in terms of strong air flow vortices. Although mine has not done a proper cobra, it can fly around and turn at a really steep angle of attack, a bit shy of 180, because of the extreme symmetry of air flow and strong vortices. The less swept/more "conventional" types of wings definitely have more air flow issues at high angles of attack and need more engineering to get them to do a lot of drastic high alpha.The big problem with the cobra maneuver is keeping the flow across both wings symmetric at the 180+ degree AOA.
Typically what happens at an AOA over about ~45 degrees is that the flow over the wings becomes increasingly unstable and one wing's lift decreases relative to the other (usually very quickly). This causes the aircraft to roll and "fall out of" the maneuver with most/all of the control surfaces ineffective (aka "depart controlled flight").
Even getting up to 45 degrees AOA takes some careful aerodynamic design. Probably the most common device on fighters these days is the Leading Edge Wing Root Extension" (LERX). The F-18 is one of the most obvious applications.
At very high AOA, the extremely high sweep-angle of the LERX generates a strong vortex that washes up over the top of the main-wing and maintains attached/stable flow.
Well, Ben designed them so well...