![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#1
|
|||
|
|||
![]()
So... how strong is your wing?
The only sure way to know is to TEST it. How do we do that? We roll the airframe over on it's nose, support the main spar with a structure of some sort... Douglas Fir 2x4's works okay... then we stack a known weight onto the wing. Still confused? No problem; just follow me through. We already know what the bird weighs., thanks to all those imaginary flights out to Catalina and back. Empty weight is 318 pounds.. Nine gallons of gasoline is 54 pounds and one sorta-skinny pilot is 155 pounds, so we've got 318 + 54 + 155 = 527 pounds... and we wanna see if the wing will support 527 pounds. (Yeah, I know... lemme work up to it.) Start by removing the spinner and the prop, then bolt-on a wooden bolster that weighs exactly the same as the spinner & prop. Now we whistle-up some help and we ever to gently roll the plane forward, first onto the bolster and then onto the support structure that pokes up into the cockpit and bears against the main spar about where my legs would go. The structure is kinda high because we dont want the vertical stabilizer to touch the driveway. But we finally get it rolled over and supported on the structure we've made (now THERE was a fun project). Is it level? We check it out. Then we position a couple of yard-sticks just off each wing tip. Now we cover the wing with cardboard and start stacking on the weight. What kinda weight? Well... back in the Good Ol' Days, whenever that was, our local EAA chapter would have a couple thousand pounds of lead weights all neatly marked in matching pairs, and they'd deliver it and bust their backs helping you do the Static Test (which doesn't have anything to do with radio). Nowadays your best bet is probably bags of Portland cement or other building material ( ...such as Plaster Sand... ) available in bags, each marked with the weight of the contents. ( Anywhere outside of the USA it'll probably be marked in kilograms instead of pounds. Not a probelm; just work it out. ) Now you lay the weights onto the protected surface of the upside-down wing, starting in the middle and working your way out toward the tips. Five hundred and twenty-seven pounds is about six bags of Portland cement so you'd have three bags per side. Out at the wing tips, the marker aligned with your yard-sticks (meter sticks across the pond) probably won't show any deflection at all. Five hundred and sixty-four pounds ( that is, six times 94 ) equals one g, which means you are cruizing along in level flight. So what's your plane rated for? If it's non-aerobatic it's probably rated for Utility Class, which is about 3.3g, Which means 3.3 times 517 or about 1706 pounds. Which happens to be about 18 bags of Portland cement, so that's what you stack on, starting at the middle and working your way out toward the tips, keeping an eye on those yard sticks. Odds are, you won't have any problem at 3.3g's -- the wing probably won't deflect at all. Now all you've got to do is take a buncha pictures and get everyone to sign the log. Or you could keep piling on the weight until something breaks. That would indicate the Ultimate Load for that particular structure but you gotta be careful dealing with that amount of weight, especially if you're working in somebody elses hangar, because when something fails it's liable to flip those bags of cement around like a frisbee. --------------------------------------------------------------------------- A lot of times you aren't working with a finished airframe; lots of times you'll only be working with a part of an airplane, such as it's horizontal stabilizer, or perhaps an engine mount., That's when things can get interesting, because you may be trying to achieve 8 or 9 g's. That's when you'll want to have a couple of video cameras running, because when the failure occurs it's liable to happen fast. Sometimes you may be testing nothing more than a main spar, probably bolted to a fixture you've designed to support it. If the main spar is made of wood there's a good chance that you've fabricated this sample out of something less expensive than Sitka Spruce and aviation plywood. Or you could be testing the strength of a part with the wood at a different orientation. (Which is what this message was all about to begin with.) :-) Gravity and persistence can teach you a good deal about aeronautics without ever leaving the ground. You'll have to fabricate your supporting structure and line-up a suitable supply of weight, but having done so you may find there is more to aeronautics than you realized... I'll leave the next step up to you because when you get right down to it, YOU are the mechanic-in-charge. -R.S.Hoover |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
CHEAP Los Angeles C-172 Flying Club CHEAP | [email protected] | Aviation Marketplace | 7 | May 7th 09 03:32 PM |
CHEAP Los Angeles C-172 Flying Club CHEAP | [email protected] | Owning | 1 | May 7th 09 03:32 PM |
CHEAP Los Angeles C-172 Flying Club CHEAP | Sunho | Owning | 2 | May 7th 09 12:13 AM |
CHEAP Los Angeles C-172 Flying Club CHEAP | xyzzy | Owning | 0 | April 6th 09 03:31 PM |
Testing the Testing of Mogas | Jay Honeck | Piloting | 22 | July 24th 06 09:38 PM |