Do you have the sheet? I’m betting that the flexural modulus number is not pure resin…
Ok, I looked it up after typing a bunch of stuf… http://www.axson-technologies.com/sites/default/files/TDS%20-%20Marine%20820%20160524_1.pdf
I think this is the right resin?
It’s not a neat or cast pure resin sample for the felxural modulus testing… there is no given information as to the type of reinforcement or amount. The tests that have the asterisk on them are the ones done with resin only. This is why using the TDS to determine the best resin is a bit of a hit an miss type of thing… if they did the test panel with all ultra high modulus unidirectional fiber with a very low resin content, the test will look much better. You might be able to call them and ask about the specimen, they might be able to tell you so you have a better picture of what the test data reveals.
here is another tds for a resin sytem that I use for comparison on how different they can be: http://www.tencate.com/emea/Images/TC250_DS_012417_Web28-3802.pdf
this tds has a ton more information but not everything that you might want… This is why we end up doing test panel after test panel in aerospace. The design margins are pretty tight and making things wider will only end up in a heavier part than necessary… also when it comes to certified craft, this sort of stuff can carry heavy liability in the event of lives lost or damage done.
I’m not sure if I’m helping at this point or just throwing too much information out… lol
I guess in direct response, No the material your using would probably not give stiffer part than the pt5760 considering the 5750 lists the flex at 3,057,938 psi using glass reinforcement and 7,304,718 psi with carbon fiber. Both number being considerably higher than the adtech sheet lists. There are still many other resins out there that probably are better than the one I thought of off the top of my head. Though each have different strengths and weaknesses as well as price. Choosing what is the right material is one of the hard parts. Ultimately you use what you have or can get and go with that until it fails you in one way or another. You can see though how the reinforcement makes such a huge difference, in this example a 2x increase in flexural modulus by going from glass to carbon fiber. You could probably go even higher with ultra high mod uni.
For your part I would expect that you use much unidirectional? I would think the resin would have some effect for sure, but the reinforcement should be providing the majority of the stiffness. Maybe use ultra high mod uni? Also the geometry is going to greatly effect stiffness. Having a flat piece of uni that is 100 plys thick probably wont be as strong as using a C Chanel or box shape. The wing spars are like this and have such a shape but still have an expected deflection, inches, at max load.
It sounds like you’re trying to squeeze out as much as possible? How are you measuring deflection now? And what is your target? Is budget an issue? How many do you need to make?