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80" Cap 232 Modifications
I am planning on scratch building an 80" Cap based on the Midwest kit plans. Outlines will be the same, but everything will be lighter (based on discussion with Dick Hanson). I would also like to lower the horizontal stab some to reduce the pitch and roll coupling with rudder. My questions are:
1) How much to lower the stab? I am thinking maybe 1-1.5". Any more than that and it will start to look goofy and decidedly non-scale. Can much of the pitch couple be trimmed out with CofG changes as well? I don't need perfection, but less is always better and easier to mix out with no weird side effects. 2) The roll couple should be manageable with a change in dihedral (I think). Any guesses on how much to take out? 3) I would like some recommendations for aftermarket landing gear (carbon fiber preferred) and a fiberglass cowl to keep the weight down and quality up. I plan to use a two piece wing with carbon joiner tube, so I might as well continue the carbon theme.;) I will be using sheeted foam core wings and stab and a built up balsa fuse. My target is less than 12lb with a ST2300 or OS160 for power. Any other tips/things to note about this aircraft or the Midwest plans? Thanks, Mark |
RE: 80" Cap 232 Modifications
You may want to take a look at some pics of a Carden 40% Cap and see where they placed the stab. If I am not mistaken, GP has a .40 size cap kit and in the instructions they stated that the dihidral was more than scale and not to change it as it would adversly effect roll coupling. A chat with Peter Goldsmith may prove useful as well.
Shawn |
RE: 80" Cap 232 Modifications
FWIW the Cap stab -in the scale location works extremely well -the lowered stabs are easier to do structurally and I have done them in various positions for that reason. but the benifits of lowering it for any real performance gain -- in my book -- extremely questionable - read that horse sh-it
some excellent full scale aerobats have relatively high stabs -the Zlin 50 for example . in order of importance - weight then power then weight then power then weight then power . |
RE: 80" Cap 232 Modifications
ORIGINAL: dick Hanson FWIW the Cap stab -in the scale location works extremely well -the lowered stabs are easier to do structurally and I have done them in various positions for that reason. but the benifits of lowering it for any real performance gain -- in my book -- extremely questionable - read that horse sh-it some excellent full scale aerobats have relatively high stabs -the Zlin 50 for example . in order of importance - weight then power then weight then power then weight then power . Thanks for the input, Dick, it's been a great help. Mark |
RE: 80" Cap 232 Modifications
Lowering the stab on many CAP 232's significantly reduces the push to the belly in Knife-edge. In turn that means that you need much less rudder-to-elevator computer mix. Done this on three Cap's in the past and the latest 79" GP Cap 232 has it done already. That GP CAP pictured, KE'd very well as supplied with only a few % of mix.
Regards, Eric. |
RE: 80" Cap 232 Modifications
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RE: 80" Cap 232 Modifications
ORIGINAL: Eric.Henderson Lowering the stab on many CAP 232's significantly reduces the push to the belly in Knife-edge. In turn that means that you need much less rudder-to-elevator computer mix. Done this on three Cap's in the past and the latest 79" GP Cap 232 has it done already. That GP CAP pictured, KE'd very well as supplied with only a few % of mix. Regards, Eric. Has anyone had direct experience with the Midwest kit and it's characteristics in KE? Thanks, Mark |
RE: 80" Cap 232 Modifications
OK...this is an honest question..
I do not know much about aero or plane design... sadly,, I am one of the ARF masses.... and I have not owned a CAP... but the comments state that moving the stab made a difference... forgive me, but my question is this... unless you fly the EXACT same model with the stab in two different places.... how can you really tell if it is making a difference.. as two models of the same plane can fly quite differently due to the several hundred other things that could be a hare of here, a scosh there?? Honest question... how do you "KNOW" it made a difference? I can then add the testing methodology to my quiver of knowledge... Thanks |
RE: 80" Cap 232 Modifications
forgive me, but my question is this... unless you fly the EXACT same model with the stab in two different places.... how can you really tell if it is making a difference.. as two models of the same plane can fly quite differently due to the several hundred other things that could be a hare of here, a scosh there?? The differences between airframes you ask about are real, since no one can exactly duplicate another airframe, but those differences are small between good builders. If you had Eric build one and Dick Hanson build another, one might need 4% mix to trim out a couple and the other 6%. But it won't be 2% and 20%, which is what we are talking about by relocating the stab. Mark |
RE: 80" Cap 232 Modifications
Gentlemen,
Thank you for the input, it is now time to get over to the shop and do something with it. Going from this, I will definitely be lowering the stab for both structural and aero reasons. I will have to wing it :D on the dihedral and see what happens. If anybody has a recommendation for landing gear or cowls, please let me know. Thanks, Mark |
RE: 80" Cap 232 Modifications
Ref.
"forgive me, but my question is this... unless you fly the EXACT same model with the stab in two different places.... how can you really tell if it is making a difference.. as two models of the same plane can fly quite differently due to the several hundred other things that could be a hare of here, a scosh there?? Honest question... how do you "KNOW" it made a difference? " The way I found out about this condition was flying my CAP's, including a 321 EX. They all exhibited a wicked push to the canopy in four-point rolls and knife-edges. When a plane does not "work", out comes the knife or saw. For roll-couple I used to increase or decrease the dihedral. For elevator problems the rule of thumb was lower the stab for a push and raise for a pull. How much is a guessing came of trial and error. Also it is not a simple action and result because other things can be made worse such as pulling or pushing to the canopy in up and down lines. After 50 years of modeling you get good at guessing! As regards the Great Planes CAP 232, mine only needed a few % of up and no roll correction. It was by far the best CAP I have ever flown in many departments. Also I have never built an ARF as good as this one. Said another way, I didn't modify it. Usually I do something. Not on this one. I did fit a soft-mount but that's another story. Regards, Eric. |
RE: 80" Cap 232 Modifications
and no roll correction. Mark |
RE: 80" Cap 232 Modifications
pictures are not working - will try later...
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RE: 80" Cap 232 Modifications
Thanks all... I get it...
I was out of town for the weekend so sorry for the delayed response |
RE: 80" Cap 232 Modifications
ORIGINAL: exeter_acres Thanks all... I get it... I was out of town for the weekend so sorry for the delayed response I do not know much about aero or plane design... sadly,, I am one of the ARF masses.... Mark |
RE: 80" Cap 232 Modifications
FWIW--
the CG setups will change how the CAPS and any other bird handles But -- the stock CAP 232 setup - will do absolutely flawless four points extended slow rolls -etc.. setup correctly with very little mix The reasons why a lowered stab helps have been listed many times -by others also. frankly I can't buy into it . Having built many CAPS with large/small / high/ low stabs - there is some difference but other than structural - none I would bother with. making the stab larger makes for far greater differences in how the model performs check out your own setup -- likely the horizontal tail has been fudged a fair bit . . |
RE: 80" Cap 232 Modifications
ORIGINAL: dick Hanson FWIW-- the CG setups will change how the CAPS and any other bird handles But -- the stock CAP 232 setup - will do absolutely flawless four points extended slow rolls -etc.. setup correctly with very little mix On your lightweight ones what did you use for dihedral? Straight in line with only the taper creating dihedral, flat top of wing or somewhere in between these two? Mark |
RE: 80" Cap 232 Modifications
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Here are some pictures of the Great Planes 79" CAP 232 that illustrates the much lowered position of their stab.
I don't want to get into a brawl with Dick Hanson over this stuff. Dick is a well known designer and builder. Please take my information more as a data report for you to do with as you see fit. Regards, Eric. |
RE: 80" Cap 232 Modifications
ORIGINAL: Eric.Henderson Here are some pictures of the Great Planes 79" CAP 232 that illustrates the much lowered position of their stab. I don't want to get into a brawl with Dick Hanson over this stuff. Dick is a well known designer and builder. Please take my information more as a data report for you to do with as you see fit. I don't want a brawl, either. I'm just trying to get the best flying Cap 232 I can. I respect Dick's resume and advice and yours as well. What I do with it is up to me. As mentioned, CofG and many other set up items can influence this, even a particular flyer's choices and preferences for control throws and style of flying. There is no magic bullet for this stuff and it takes trial and error and some compromise in the end. From this discussion and other reports and comments I have seen, I will be lowering the stab some, for an easier/better structural arrangement and to reduce coupling. If it goes wrong, I will have no one to blame but myself...;) Did you ever notice the amount of dihedral used on the GP version? Thanks to all for the help, Mark |
RE: 80" Cap 232 Modifications
I have avoided the dihedral question because it is a hard one to answer.
The thicknes of the wing-rib at the root and the wing-rib at the tip means that the wing tapers a lot in thickness. Your dimensions would influence the resultant flight behavior, which I can't predict. My CAP is now in the hands of a less experienced flyer and he is doing very well with it. That also means that I can't easily measure it for you either. Regards, Eric. |
RE: 80" Cap 232 Modifications
ORIGINAL: Eric.Henderson I have avoided the dihedral question because it is a hard one to answer. Since the Cap is a low wing design, for a two piece wing would you go with a tube joiner and bolt the joined wing to the fuse or keep the tube in the fuse and slide a wing panel on from each side (as is typical on most 2M pattern ships right now)? I am leaning towards joining the wing, then bolting it on with 4 bolts myself, but that is with no experience on a plane this size so far. Which is the lighter set up? Dick, can you comment on this as well? Mark |
RE: 80" Cap 232 Modifications
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I have done this exact same size --both ways and the tube joined wing model was lightest - however that is because the entire model was -piece by piece -lighter -lighter cowl and canopy also
typically the CAPS I did this size are 10lobs with a YS140 and 13 with a ZDZ40 and can I also flew the H9 80 " setup with a ZDZ50 and a in cowl setup I designed - very good flyer but almost 3 lbs heavier The dihedral was close enough with the 10% tip and 12% root - and flat along top high point Note in the interior shot --the forward fuselage ass'yis an I beam --on it's side - this is incredibly stiff and light made from laminated balsa and spruce longerons . |
RE: 80" Cap 232 Modifications
I have done this exact same size --both ways and the tube joined wing model was lightest - however that is because the entire model was -piece by piece -lighter -lighter cowl and canopy also The dihedral was close enough with the 10% tip and 12% root - and flat along top high point Note in the interior shot --the forward fuselage ass'yis an I beam --on it's side - this is incredibly stiff and light made from laminated balsa and spruce longerons . Many thanks for the 3 view and pics. Mark |
RE: 80" Cap 232 Modifications
I showed the fuselage on it's side - - --Imagine an I beam-the sides are top and bottom -the floor in centre is the upright
Each side is laminated balsa -light stock - bonded at 90 degrees . the bulkhead is als laminated The spruce carries the load fore/aft - the floor does two things: It makes the fuselage absolutely rigid against any "racking" secondly the exhaust system is below - isolated from anything else. Frankly I think the current structures used by many ARFS - is simply archaic-- |
RE: 80" Cap 232 Modifications
I showed the fuselage on it's side - - --Imagine an I beam-the sides are top and bottom -the floor in centre is the upright Each side is laminated balsa -light stock - bonded at 90 degrees . the bulkhead is als laminated Lots to think about, thanks Dick. Anything I can do to get it to 12lb or less is very appreciated. Did you find the 10lb ones at all "floaty" or touchy in windy conditions? That is extremely light for that much wing area. Mark |
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