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SDF

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Posts posted by SDF

  1. Lets not perpetuate this nonsense. Danny is completely correct and Mal is wholly wrong. It is the leadout position wrt the CofG that matters the belcrank within reason can go anywhere. It is, however, usual to try to place the belcrank such that the rake of the lines is tangential to the arc of the lines in flight. This avoids a bend in the leadouts where they exit the wing.

  2. Erflog,

    (Looks like you spotted the error whilst I was typing)

    I think there is and error in your calculation. You appear to have multiplied the mass by the speed then squared the result making your estimate of the force a factor of ten too big.

    40 lb = 18.1kg

    30mph = 13.4m/s

    120ft = 36.6m

    18.1*(13.4^2) / 36.6 = 88.8N

    or just over 9kg

    or at 40mph just over 16kg

    But I think 40 mph might be too low a speed for such a machine to fly so it would probably still need to be tethered to the preverbial immovable object.

     

    Edited By SDF on 24/06/2013 21:53:12

  3. We had a demo at the club I used to belong to of how to glass a wing but can't remember who it was by now.

    Use laminating epoxy as already advised. Thin this as required using pure methanol. Lay the glass cloth over the wing. Don't try to use a brush. Pour the epoxy sparingly onto the cloth/wing and then use a camel hair paint roller cut down to about 2" wide to spread the epoxy. Gives really good results with just the right amount of epoxy to properly wet the cloth without excessive weight gain. Pop the roller in a jam jar of acetone before the epoxy sets and it can be reused.

  4. I could never really see the point of buddy leads. What is the problem with passing the TX between tutor and trainee? Thats how I learnt to fly. Keep it simple.

  5. You do realise Diamond is a form of carbon and will burn quite nicely. I would suggest keeping them away from the torch unless you want to buy some more.

    A (probably) cheaper alternative is a bit of brass tube sharpened at the end with knife.

  6. BEB, I see what you mean but the dynamic imbalance is likely to be very small as blade thickness is small compared to the diameter so the scope for misalignment of the pricipal axis is, I would have thought, quite limited. This would probably also show up as a static imbalance with the prop vertical, but I don't suppose may people check the balance of their prop in that orientation.

    Erflog, I suspect the vibration would damp out pretty fast without any stimulus but can't be sure. Might be an interesting exercise to try and computer model it, not done any of that for a while.

    The kineic energy of the blades may be different but I think that only becomes relevant when you try to change it. Same effect as the angular acceleration I described.

    Could your post arrival vibration problem be due to a partial failure in the internal model structure making it more flexible than intended.

    I have a control-line twin (same configuration as a F82) with two diesels and on the ground there is a beat frequency oscillation when both motors are running that makes the two fuselages forward of the wing visibly flex from side to side quite alarmingly but there is no problem in the air. Funny old stuff vibration.

  7. Erfolg, Interesting paper on balancing rotors. Not really sure what your getting at with the parallel axis theorem though. It just says if you rotate a body about its centre of mass the moment of inertia is a minimum about a given axis. Our staically balanced prop is being rotated about its centre of mass.

    Say our staically balanced prop has the mass distributed so there is a lump of mass M at radius -2R and a lump of mass 2M at R with respect to the hub centre, i.e. one lump in each blade. Clearly not an even distribution. The centripetal acceleration at any radius (r) is given by -r*w*w (w should be omega, can't do greek i.e. the angular velocity). The acceleration is linear along the blade in the rotating axis set so the net force (F=ma) at the shaft is 2R*w*w*M - R*w*w*2M = 0. No out of balance. So the radial distribution of mass doesn't matter a jot at fixed RPM and single bladed props and bob weights work fine.

    Under angular acceleration (changing RPM) there is an out of balance as the moment of inertia of each of our two lumps of mass is proportional to the square of their respective radii from the hub. There is a net force perpendicular to the axis along the blades as a result of the uneven torques required to achieve the same angular acceleration. Don't know how significant this effect might be but I suspect small on a normal prop.

    There could also be a coupled moment perpendicular to the axis of rotation if the masses are not evenly distributed throught the thickness of the blade (principal axis misalignment). The same effect as the car wheel dynamic balance already mentioned. As the blade thickness is small compared to the diameter the misalingment is likely to be very small and I wouldn't expect this to be a significant effect.

    I shall look forward to reading the article to seeing what it actually says.

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