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ENGINE DOWN THRUST ANGLE QUESTION???

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Old 06-09-2009 | 06:52 PM
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Default ENGINE DOWN THRUST ANGLE QUESTION???

I was thinking of posting this question in Kit Building, but maybe aerodynamics might be a better choice. I am getting ready to slightly kit bash a Sig Kadet Seniorso as tousea larger engine than the original design. The plans show 6 degrees down thrust and 2 degrees right thrust to be built into the forward bulkhead/firewall. I am just curious if this amount of enginedown thrust would be applicable as the engine size is increased? Two degreesright thrust is fairly common but 6 degrees seems like a lot for downthrust.
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Old 06-09-2009 | 07:59 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

The  "theories "on down thrust  are  pretty darn subjective
 A  LOT depends on the  speeds yo like to  fly.
   Why the larger engine?
 A whim?
 essentially th model is  of  a size  and the  wing setup makes for  a lot of  climb under power
 The  huge down thrust  was likely done to  increase speed yet   hopefully provide  some force to  keep the  nose  down
You can screw around with the  speed n downthrust  and the wing saddle position till the  cows come home 
 BUT the  stock setup makes for  a gentle very ,very easy model to fly.
 My old Seniorita can quickly be trimmed  for  complete hands off  flying - it  will  do huge circles  with a gentle undulating  flight path
 meaning the model will slightly climb till speed drops back  then dive slightly  picking up speed  and  the  nose will gradually  come up  -repeat etc.. lovely  free flight  flying
 If you are after an aerobatic setup , the  basic model arrangement is  wrong  -so once you dig into  more  power for more speed  you wil end up having to  change  angles of  wing and thrust  -or just accept it is what it is.
Old 06-09-2009 | 09:11 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

Why the larger engine?
Whim?

Well actually I was looking for something in the 75 to 80 inch range that I could hopefully keep ataround 9lbs or so to put a larger four-stroke on.I wanted something similar to J-3 Cub performance. Mild acro and slow flighting in the traffic pattern. Just a plane to play with. Also, the forward fuse needed to allow the fuel tank to be placed below the thrust line by about 2 1/2 inches. One of the guys in my club was flying his Kadet Senior ARF today. The Kadet Senior was one plane I had viewed with some interest while on the SIG site. Over the years I have seen several Seniors bashed into fairly interesting and fun planes. Take out most of the dihedral, add ailerons, make the wing mount more modern, perhaps lift struts,etc. During today's conversation with the Seniorflyer, he mentioned he hada kit, NIB that he'dsell for $60. Sonow youknow how all this got started.

Being a kit, IWill be able to more easily move equip, batt, and such so as to keep the CG right without adding weight. I can strengthen the forward fuse and use thicker firewall plywood to accommodate the larger engine. Anyway, that is the present plan.

dick Hanson, I checked the plans and the flat wing bottom and stab are at 0 degrees incidence to the fuse datum line. The chord line of the wing is probably pretty close to 5 or 6 degrees up. So I guess that is why the motor is 6 degrees down. What would happen if the wing incidence and motor thrust angle were both at or near zero? Since this is going to be a taildragger, negative lift at takeoff would not be an issue.
Old 06-09-2009 | 09:28 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

You could easily raise the trailing edge 1/4" for starters - make allowances to raise it more
the flat bottom of the wing is just a referrence line.
the true zero lift line is up to at least the center of the leading edge
with good ailerons - take out all the dihedral THEN use a slightly raised position for "center "of ailerons.
keep the weight down -big chunks of wood do no good strength wise - add some beef to the fuselage sides which take th engine loads

Old 06-11-2009 | 10:44 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???



Hello;
Piped .60? Mine has one on it and it fly's good on 0 down thrust.  (set it up as a pattern ship...lol)...what ya have to be careful of  is the wing blowing...(it took a couple of wings to get the wing strong enough).   She will do OK if you just keep it slow and don't go crazy with her...
Steve</p>
Old 08-04-2009 | 04:46 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

Hi All
I have a Sig LT 25 that I just converted to e flight..It use to fly with an OS 25FX.
Now with the electric motor it wants to climb..I added some washers behind the mount for added down thrust and it still wants to climb. I check the engine down thrust agaisnt the plans and motor seems prefect.
Could IT be a matter of the Cg being tail heavy? I balanced It on the main wing spar as per the building instructions.

THanks Dan
PS the wing chord is 12" and the wing spar is 3 1/2" form the leading edge.Thats what wasa called for in the instructions.
Old 08-06-2009 | 04:10 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

Hi All Where did all the help go?? I finally got the LT 25 dialed in.. It was more of CG problem then a dwon thrust problem.

Dan
Old 08-06-2009 | 06:29 PM
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Default RE: ENGINE DOWN THRUST ANGLE QUESTION???

It's summer, we were probably all out enjoying it....

Sounds like you figured it out for yourself. As you found the amount of downthrust required is actually linked to the CG location and the wing to stabilizer angle. The further back the CG and less the angle the lower the tendency is for the design to pitch up with a speed increase. Taken to major extremes you'll find that a 0-0-0 model with the CG located right on the neutral point does not need any downthrust and won't nose up when the speed increases. Trainers with forward'ish CG's and strong wing to stab decalage angles greatly benefit from having some downthrust.

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