Best viewed with Red and Blue 3D Glasses. A little project my co-worker Sean and I put together that I re-made for your 3D viewing pleasure. Be sure to view in High Definition.
Animation is in error,Shows no real push over, Blades have no "Coning" and cyclic input,after a tail strike the yaw rate is higher during break up phase of accicent. See Franks safty course its better.
This fails to show the cause of the negative low G pushover, what would happen in reality is the cyclic is pulled back then pushed forward aggressively causing the above effect
@7249xxl Avoiding the low "G" condition is paramount, followed by no abrupt control movements. However, if a roll is encountered, do not apply opposite cyclic to stop the roll until the rotor is reloaded. Gentle aft cyclic is ok to reload the rotor. The is is based on RHC's guidance on the subject, since there is no flight testing regimen for low "G" conditions; avoidance is key by limiting abrupt control movements (particularly foreward), intentional low "G" entries and severe turbulence.
I noticed your rotor disk does not tilt at all during the low-G entry, but the fuselage tucks nose low. The real hazard is the rolling that comes with the low-G, caused by the tail rotor thrust above the vertical center of gravity, which cannot be corrected with the cyclic at low-G.
Una grandissima stronzata!!
MrCanocia 6 months ago
you cant do "in face flying 3d effects" without making focus on them!
hackerisslv 8 months ago
Animation is in error,Shows no real push over, Blades have no "Coning" and cyclic input,after a tail strike the yaw rate is higher during break up phase of accicent. See Franks safty course its better.
hillberg100 10 months ago
So that's why my tail rotor was missing!! All this time I thought it was sky thieves!!
ESOTERICKPLAN 10 months ago
This fails to show the cause of the negative low G pushover, what would happen in reality is the cyclic is pulled back then pushed forward aggressively causing the above effect
readyornot2198 1 year ago
@7249xxl Avoiding the low "G" condition is paramount, followed by no abrupt control movements. However, if a roll is encountered, do not apply opposite cyclic to stop the roll until the rotor is reloaded. Gentle aft cyclic is ok to reload the rotor. The is is based on RHC's guidance on the subject, since there is no flight testing regimen for low "G" conditions; avoidance is key by limiting abrupt control movements (particularly foreward), intentional low "G" entries and severe turbulence.
rotorznwingz 1 year ago
@rotorznwingz so what u say is dont roll otherwyse u might wil die
7249xxl 1 year ago
I noticed your rotor disk does not tilt at all during the low-G entry, but the fuselage tucks nose low. The real hazard is the rolling that comes with the low-G, caused by the tail rotor thrust above the vertical center of gravity, which cannot be corrected with the cyclic at low-G.
rotorznwingz 2 years ago
I'd hate to be in that Robbie.
motokid032 2 years ago
this video look oddly familiar... i wonder where you got it lol rob ryder will smack you lol wish i had some 3d glasses, looks like it would be sweet
22640cal 2 years ago