What's new
Aloft Forums

Welcome to Aloft Forums. Register a free account today to become a member! Once signed in, you'll be able to participate on this site by adding your own topics and posts, as well as connect with other members through your own private inbox!

Sine wave spar

Konrad asked if there was a white paper on the subject. This thread was introduced to clear up a plethora of confusion about the sine spar. It was an invitation to ask questions about the subject and I mentioned a similar structure I had and thought was relevant and interesting.

You have alluded to having test results. Maybe it is time to organize the testing results and present a paper on the subject as it relates to this discussion. Nothing like measurements to help gain understanding. I like the thought of loading wing samples for both bending and torques as you briefly described. I would look forward to studying the model specific situation. I am not looking to start another discussion and there are already books on the subject. Rather than ask an unfocused question I plan on looking through the technical literature to see if I can find a few appropriate references that speak to me.
 
Konrad asked if there was a white paper on the subject. This thread was introduced to clear up a plethora of confusion about the sine spar. It was an invitation to ask questions about the subject and I mentioned a similar structure I had and thought was relevant and interesting.

You have alluded to having test results. Maybe it is time to organize the testing results and present a paper on the subject as it relates to this discussion. Nothing like measurements to help gain understanding. I like the thought of loading wing samples for both bending and torques as you briefly described. I would look forward to studying the model specific situation. I am not looking to start another discussion and there are already books on the subject. Rather than ask an unfocused question I plan on looking through the technical literature to see if I can find a few appropriate references that speak to me.

Rather than ask an unfocused question I plan on looking through the technical literature to see if I can find a few appropriate references that speak to me.

Fantastic idea, Salt.

Doc
 
Some remarks in RED
My thought with the CNC mill is that a sine shaped web could be easily produced. A machinist would not have to be really good at turning handles on a manual mill to get that particular shape. (Not true) A program could be produced to cut a particular profile, sine or something similar. I have no doubt that there are various machines capable of cutting the profile.

It was not apparent to me that the spirit here was to contrast a dual beam (Box?) spar with a sine spar when I started reviewing the thread. It took a number of questions before that became more clear. I beams and various structures and sleeves were discussed as well making it difficult to recognize the central theme. (The landscaping retaining wall was the only discussion that was way off topic. Yes, we got into a bit of a discussion as to the limitation of beams as we currently see them constructed in our composite wings).

The discussion now assumes a carbon fiber based material and some sort of resin matrix to keep the fiber in line (appropriately arranged). The direction of the fiber can be thought of as analogous to wood grain with various weave and tow patterns possible. The comment was made that controlling the fiber configuration was one of the drivers for the use of adhesive in the construction. (It was? this is false) My question is what would that ideal configuration look like? (There is no Ideal configuration. we would need a lot more information about how the beam was expected to perform)

My experience is that corners in structures can lead to unexpected failures and hence the mention of fillets. It was also mentioned that increased surface area could enhance adhesive performance. (I think you are confusing two issue here. Adhesive performance is measure force over area. So if the beam fails at the part line add more area to allow for more adhesive. More area improves the beam performance not the adhesive performance) I mentioned fillets for both reasons.

I would agree, my questions are also about the basic performance of beams.
A legitimate topic for another thread.

As communication takes at least two , I have to ask how could I have made it any clearer as to the intent of this thread. I think the first 2 paragraphs clearly state my aims.

I was not planing to get into the nuances of machining. There are a host of tools that most folks haven't been exposed to outside of high school tech shop (too bad most of these shop classes are now gone).

I tried to say that any beam assuming that construction methods are the same would be inferior to the sine wave spar, if the material mass was normalized. So the material had no effect on the beams performance between the samples. It was just the geometries of the beam I wanted to look at when trying to explain the performance advantage of the sine wave spar.

In this forum it was natural for the discussion to move to the HSWS and was again eluded to with my comment that guys on the slope don't seem to understand it.

Hammond moved the discussion into the practical realm with his discussion of how he implements the SWS into his aircraft. I mentioned that with the sine wave spar the adding of fiber across the part line is much more difficult with the SWS than the classic box spar. I then mentioned the Boeing patented process.

Corner fillet performance is fully understood so there really aren't any unexpected failures. Improperly manufacturer spars will suffer premature failure.

No the discussion hasn't assumed composite construction. And no the fiber in composite construction shouldn't be thought as being analogous to wood grain unless the tree can be grown in the shape of the end product. (This can be done and has been done with support structures as seen in Old Iron Sides).

Please note that Doc and I try our best to not get bogged down in math (detailed engineering) on this forum. This is not an engineering journal. (BTW I was an aerospace engineer and Doc has his PHD as a material scientist). We both are aware of how quickly we could loose many reading these posts if we got into formulas to make our points. So while we may keep things at the conceptual level we aren't doing it to be condescending to anyone. We are just trying to give as many folks as possible a basic understanding of the issue being discussed. I try to give reference material so that somebody can dig deeper into any subject I'm discussing. If you think Doc and I see thing the same you might want to read some of the heated topics we get into.

All the best,
Konrad
 
Last edited:
Konrad asked if there was a white paper on the subject. This thread was introduced to clear up a plethora of confusion about the sine spar. It was an invitation to ask questions about the subject and I mentioned a similar structure I had and thought was relevant and interesting.

You have alluded to having test results. Maybe it is time to organize the testing results and present a paper on the subject as it relates to this discussion. Nothing like measurements to help gain understanding. I like the thought of loading wing samples for both bending and torques as you briefly described. I would look forward to studying the model specific situation. I am not looking to start another discussion and there are already books on the subject. Rather than ask an unfocused question I plan on looking through the technical literature to see if I can find a few appropriate references that speak to me.
Konrad asked for a white paper because he didn't want to write one if there was one already published. The Sine Wave Beam is well understood in the engineering literature. It just hasn't been seen much in our toys. I'm not sure there is a plethora of confusion about the sine wave spar. I think many folks just don't know what it is and how it differs from the concept of an I beam they may have learned in high school.

What I wanted to discus at a very high level (conceptual) was why the sine wave spar was superior to most structures we see in the wings of our toys. I did not want to write a basic introductory level discussion on how beams work. We left out volumes and scores of other configuration. In this forum I wanted to look at the sine wave spar as it has been introduced into our hobby, That means the Aeroic molded wings.

All the best,
Konrad
 
Last edited:
Quote:

"If you think Doc and I see thing the same you might want to read some of the heated topics we get into."

No we don't. Its a simple case of mind over matter - I don't mind, and you dont matter...


images-35.jpeg
images-28.jpeg

Doc.
 
Here is another take on the SWS. I was given a Bridi Tercel 50" HLG. I built one of these in my youth. I hope to add some improvements. Key is to lengthen the span from 50" to 60" (1.5m). This added 20% in span is giving me some concern with the spar. (Not really) So to add some torsional strength I laid the shear webs to mimic a SWS. Yes, the spar might actually be weaker in bending moment as there is about 50% less glue area with the webs as there was with the as drawn "C" spar.
Tercel SWS.jpg
 
How are you calculating that there is 50% less glue area? Is that because the spars are twice as high as the sheer webs are thick? The webs are technically longer than stock so it's probably not quite 50% less glue surface. Looks good. I should build my Tercel kit. I too had one as a teenager and when i found the wing i saw how many building mistakes i had made i was surprised the glider flew as well as it did. Proving again that most airframes are probably over designed.

Hank
 
You are thinking correctly. Now that you have called me on it. The spars are 3/32 not 1/8 thick.
 
reminds me of these walls:
"Popularized in England, ... crinkle crankle wall, also known as a crinkum crankum, sinusoidal, serpentine, ribbon or wavy wall, is an unusual type of structural or garden wall built in a serpentine shape with alternating curves"
 

Attachments

  • 254972823_194760642828633_7026424203345932692_n.jpg
    254972823_194760642828633_7026424203345932692_n.jpg
    59.6 KB · Views: 145
reminds me of these walls:
"Popularized in England, ... crinkle crankle wall, also known as a crinkum crankum, sinusoidal, serpentine, ribbon or wavy wall, is an unusual type of structural or garden wall built in a serpentine shape with alternating curves"
Easier than trying to make a straight wall. (Harder for the eye to see flaws). They might hold up to wind loads better. But I think it is just a fashion thing.
 
Easier than trying to make a straight wall. (Harder for the eye to see flaws). They might hold up to wind loads better. But I think it is just a fashion thing.
Not at all. Single brick walls fall over, double layer takes twice the material. This was the compromise, highly practical, and the effectiveness is proven by their age.
 
Said much the same in post 21.

But how does the art of laying bricks impact load beams, particularly in tension?
 
in the limit, more webbing may be added , forming new rigid triangles :
 

Attachments

  • webbed Tercel SWS.jpg
    webbed Tercel SWS.jpg
    479.6 KB · Views: 156
You are showing is a box spar. I think Anthony Fokker did this first with the F1 (triplane).

Your spar is much stronger but also heavier.

Bridi with the “C” spar was looking to make an “I” beam that was less critical to manufacturing issues (fitting the web between the spar caps).
 
Konrad,

Are you gonna start a thread on the Tercel?

Aside from the spar modification. I’m curious why you want to increase the span. And where you are gonna add it? A few inches to each section I suppose. Or a 10” flat section in the center?

Hank
 
Wasn't think of it. Now if you do, I'll tag along. It might help me stay motivated. I need to do a classic wood build as I'm working on so much broken glass!

As I recall increasing the span improves the efficiency by the square of the span. (I'd need to dig up some formulas to be sure of the relationship) This is why we say the best way to improve a sailplane's performance is to move the wing tips further apart.

I recall the 60" ships just out flew these small 50" HLG gliders. I'll be adding another 5 inch panel to the tips and changing the planform to look more like the Schuemann layout.
 
Last edited:
Hey Konrad,

I probably won’t start the Tercel for sometime. My next big project is to finish organizing my garage and rebuilding my workbench to function better. I was thinking the next project I’d start would be the 2M REStart I got from Wayne. I promised him I would do a thread on that one.

Hank
 
Back
Top