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Old 09-25-2013 | 04:03 AM
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sensei
 
Joined: Jul 2002
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From: SAN ANTONIO, TX
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[QUOTE=jordanorville;11623756]I am building a 108" C-130 from scratch. This bird will have retracts, brakes, fowler flaps, functioning ramp/door, cargo rails, and will be used to airdrop pallets, Jeeps, ect. I am quite a ways into the build and have several questions.
1. This aircraft will have a modified flat bottom airfoil, a wingspan of 108", a chord of 12.5" and about 2.5" of camber. I don't want to overbuild this thing but am worried about the overall strength as I have never done a complete scratch build. It goes without saying but i have no intentions of pulling high g`s in this bird.

My initial thought is to make a 1 piece detachable wing using 2 parallel boxed spars, one 3" aft and one 9" aft. This is very similar to the actual aircraft except it uses I-beam spars and the outer wings detach outboard of the #2 and 3 engines. I would love to set up mine to detach the same way but don`t want to create a weak point or add the excess weigh of aluminum tubes or carbon rods. I was planning to use 3/8x1/4 or 1/2x1/4 hardwood for the upper and lower parts of the spar and 1/8 balsa for sheer web. I am hoping that someone with a little more experience could give me some insight, i would estimate that the fuselage will weigh between 8 and 10 lbs. fully sheeted with radio and servos. all of the fuel/batteries will be in the wing aft of each engine or in the aft nacelle, this should help with wing flex a bit. This brings me to my second question

2. Power plant: First of all i need to decide how much thrust i will need, I planed to use 4x .25 or .35 glow motors, however i am terrified of syncing and keeping 4 glow motors running. I also thought of using 4 electrics for reliability but have ZERO experience with them. Thoughts?

How about this, use 1/2" x 1/4" strait grain spruce upper and lower spar caps, but span wise taper them from 1/2' thick through the center section to 1/8" thick at the tips. This would allow you have the strength you need for flight and allow you to lose weight as you move towards the tips and the load diminishes. I would also glue in 1/4" x 1/8" hardwood verticals throughout it's length and then sheet both sides of the spar with medium density 1/16" thick balsa sheeting as webs.

Bob

Last edited by sensei; 09-25-2013 at 04:06 AM.