WHAT??? ...I thought the "old-forum" - was preserved here in the archives!!As I recall there used to be quite a few issues about design on the old Forum. Too bad it is no longer available.
Here is two from the Old Forum. I did a search for Craig Wall and came up with nothing. When ever I found something interesting on the older forum I would save it to my computer.WHAT??? ...I thought the "old-forum" - was preserved here in the archives!!
I know the search-engine/ feature here is worthless!
There ARE a LOT of forums and topics here now.... it should be doable to a determined scroller to find old threads on designs!
I am making RC scaled down model of AS350 b3 heli... I have worked out many things in my head and currently working on its MGB but one thing i am stuck with is that how to vary tail rotor pitch to catter for the torque variation in main rotor. Electric motor as a tail rotor via electronic gyro is an option but I want it to be close to original design ( plus save the power ). As an aerospace engineer i have passed papers(until now i havnt seen any practical use of even the Cl (coefficent of lift) what to say of the Thermodynamics and compressible flow ). What i am doing is what I have been doing since childhood.I have learned a great deal on the Rotary Wing Forum about design, building and safety of gyroplanes.
I am not an aerospace engineer.
I cannot answer your questions or debate your theories if I don’t know what they are.
If you have specific questions; please articulate them Ziad Khan.
As an aerospace engineer you should have learned how to do that.
If you ask good questions you may get good answers.
Early RC heli's were almost un-flyable due to manual controls, the 80's saw the introduction of "rate gyros" that dampened the yaw very significantly, but they do tend to drift a bit.I am making RC scaled down model of AS350 b3 heli... I have worked out many things in my head and currently working on its MGB but one thing i am stuck with is that how to vary tail rotor pitch to catter for the torque variation in main rotor. Electric motor as a tail rotor via electronic gyro is an option but I want it to be close to original design ( plus save the power ). As an aerospace engineer i have passed papers(until now i havnt seen any practical use of even the Cl (coefficent of lift) what to say of the Thermodynamics and compressible flow ). What i am doing is what I have been doing since childhood.
I'm with you Eagle. I have a part fantasy, part technical question to ask. Imagine a 4 blade set in which the blades cannot flex up nor down(fantasy?}. Now take another set that will rotate in the opposite direction and place it on the same vernicle axis to form contra rotational pair. How close can they be to each other so that the lower set does not cause the upper set to fail producing lift?(technical). Anybody?Why is there no design thread / debate here on Rotary forum. i had joined it purely for design info sharing but i am disappointed that no info here !
I'm with you Eagle. I have a part fantasy, part technical question to ask. Imagine a 4 blade set in which the blades cannot flex up nor down(fantasy?}. Now take another set that will rotate in the opposite direction and place it on the same vernicle axis to form contra rotational pair. How close can they be to each other so that the lower set does not cause the upper set to fail producing lift?(technical). Anybody?
Dream on. This is from a NACA film about 1955 from the rotorhead of a Sikorsky S-56, I think. Sorry about the German - couldn't find the English version. Rotate the image 90 degrees to see the behavior.when there is rotation there will be no flex due to centrifugal force regidity. you can simlate it and assistant on the site are very helpful