I thought it was the Phast Phrog! 😀The Super Phrog, Boeing Vertol 360.
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I thought it was the Phast Phrog! 😀The Super Phrog, Boeing Vertol 360.
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The video from Greg’s airplanes was set in 1943 - so an F4U-1 time frame. The American fighters compared quite well, alot to be said for the massive R-2800.Sorry to quote Tom Cruise, but it’s not the aircraft, it’s the pilot! The average naval aviator of late ‘44 or early ‘45 would have had vastly more experience than the average Luftwaffe pilot. An interesting way to look at it this…the P-51 (and good pilots) proved to be a superior design to German models but the Corsair proved to be superior to the P-51 during the “Football War!” On a more serious note, you can read about the Navy’s analysis (1944) of the two aircraft from the Pax River team here, https://militaryhistorynow.com/2021...-up-between-the-two-fighters/#google_vignette it briefly notes testing that was done against some axis fighters…both the Corsair and Hellcat could turn inside the German models, something the P-51 could not do.
It was denied as “not service connected”.I’d like to see the VA disability claim for hearing from those nacelle gunners!
The quality of the box matters little. Success depends upon the man who sits in it.Sorry to quote Tom Cruise, but it’s not the aircraft, it’s the pilot!
The quality of the box matters little. Success depends upon the man who sits in it.
Manfred von Richthofen
During the '80s the Soviet Union designed, but never build a huge heavy lift tri-rotor helicopter.
The MI-32 would have been larger than an Airbus A320, with a max takeoff weight of 140T with a 60T payload.
With this rotor configuration and overall aircraft mass, it would have been extremely stable in a hover.
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Would it have been stable, though?During the '80s the Soviet Union designed, but never build a huge heavy lift tri-rotor helicopter.
The MI-32 would have been larger than an Airbus A320, with a max takeoff weight of 140T with a 60T payload.
With this rotor configuration and overall aircraft mass, it would have been extremely stable in a hover.
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Drones will be doing this in the future. We just need to sit back and k and enjoy another slurpee.It seems to me that figuring out a sling load lifting point (or points) would be complicated.
We actually worked on 3 rotor multi-rotor control designs here for a bit, demonstrating we could train an AI autopilot to operate one. We picked the 3 rotor design because it is a hard problem. Much more complicated than a 2 or 4 rotor design problem, oddly enough. Balancing the lift and torque is not simple.Would it have been stable, though?
With 3 rotors it still has unbalanced torque, plus you’re going to get some strange wake interactions and effects of gyroscopic phasing.
One of several papers on the subject, doesn't seem to much of an issue.With 3 rotors it still has unbalanced torque, plus you’re going to get some strange wake interactions and effects of gyroscopic phasing.
Well, they are kind of cheating by adding a servo that tilts one (or more?) of the rotors. Last sentence in conclusion.One of several papers on the subject, doesn't seem to much of an issue.