blackkite
Don't laugh, don't cry, don't even curse, but.....
- Joined
- 31 May 2007
- Messages
- 8,574
- Reaction score
- 6,765
hartmutbehrendt said:Hello, the following for some interessest:
Josef has built this plane by using plywood, spruce stringer, balsawood, glass- and carbon fibre, and a lot of styropor. He has prepared a huge number of moulds to fabricate all the cfc parts.
The front engine is a Seidel ST 710, the rear one a Seidel ST 7-70.
Menz propeller at front 22/12, rear Menz 22/12 L, static RPM on ground 5200 RPM.
Wingspan 300 cm, Length 265 cm, dry weight 23.5 kg, No lead required for balancing.
Functions: elevator, rudder, aileron, jointly and separately controlled engines, 4 split flaps as landing aid, proportional pneumatic brakes, retractable landing gear specially made at Wabo, 8 cooling flaps for front engine (servo operated), electrically operated canopy, 2 indipendend glowplug electronic systems, for each engine one, made at Microsens, 17 servos, Futaba S-Bus servo wiring.
Plans increased three-side-view from internet. His drawn out detailed designs on this plans are not clearly visible and understandable, and so not suitable for publication.
Josef will never sell this model.
Regards, Hartmut
Thanks for detail information. Really outstanding exact shape RC model.hartmutbehrendt said:Hello, the following for some interessest:
Josef has built this plane by using plywood, spruce stringer, balsawood, glass- and carbon fibre, and a lot of styropor. He has prepared a huge number of moulds to fabricate all the cfc parts.
The front engine is a Seidel ST 710, the rear one a Seidel ST 7-70.
Menz propeller at front 22/12, rear Menz 22/12 L, static RPM on ground 5200 RPM.
Wingspan 300 cm, Length 265 cm, dry weight 23.5 kg, No lead required for balancing.
Functions: elevator, rudder, aileron, jointly and separately controlled engines, 4 split flaps as landing aid, proportional pneumatic brakes, retractable landing gear specially made at Wabo, 8 cooling flaps for front engine (servo operated), electrically operated canopy, 2 indipendend glowplug electronic systems, for each engine one, made at Microsens, 17 servos, Futaba S-Bus servo wiring.
Plans increased three-side-view from internet. His drawn out detailed designs on this plans are not clearly visible and understandable, and so not suitable for publication.
Josef will never sell this model.
Regards, Hartmut
Jemiba said:Welcome here Hartmut and thanks for those explanations. Yes, Josefs model is more,
than just an oob "Schaumwaffel" (foam wafer, fully depron models and the like) and it's
good staged by you, too. Always "Hals- und Beinbruch" for him as his model (Or are there
other greetings in the model scene ?) !
hartmutbehrendt said:In the flying world we say 'Holm- und Rippenbruch', ...
hartmutbehrendt said:..the area before the CG, seen from the side view, is greater than the area behind, ..
Oh clever approach! Good luck to you.hartmutbehrendt said::'(Hi Blackkite, Josef and me we know this video already, thank you. We are thinking about the circumstances for the crash. This video is the reason that josef has delayed the first flight of his Shinden. He plans to built a smaller Shinden first to try the behavior. I myself I think that the area before the CG, seen from the side view, is greater than the area behind, the crash showes typical indizes for this matter, Hartmut
hartmutbehrendt said:...If the Square meter before the CG is higher than after the CG, seen from the side of the model, the vertical stabilization around the vertical axis failes.
blackkite said:
If this model airplane's angle of attack becomes large at a low speed, front wing stall and generate rapid head lowering occur this airplane?
Thanks a lot. Your explanation is little hard for me. I need more study about canard aircraft flight chracteristic.Bill Walker said:This depends on your definition of "stall". The main wing of a canard design is hard (but not impossible) to stall. The aircraft may have rotational momentum in the pitch axis at the time the foreplane stalls, allowing it to continue briefly pitching nose up, enough to stall the main wing.
Stalling the foreplane can result in a loss of pitch control that can only be overcome by changing the pitch. This is a bad situation to be in. You hope that the stall of the foreplane is accompanied by a nose drop, but it may not always be so, or it may not always be fast enough, or it may be too fast. Also note that if the nose pitches down to unstall the foreplane you are also reducing the lift coefficient of the main wing, at a time when you may not want to do this. Consider a foreplane stall on short final. An uncontrolled nose drop plus a loss of lift is probably not a good thing at that point.
I suspect this is part of the reason for the slats and double flaps on the Shinden canard. Stalling the foreplane before the mainplane is not desirable.
Thanks! Japanese Shinden simplified RC model operator said so.perttime said:From what I've read on R/C forums, canard models can be very sensitive to CG location. They can fly very well but you have to get the setup right.
Jemiba said:"Fugaku still attacking !" ;D
blackkite said: