Fishdude said..
FWIW The test rig in the above Doc looks flawed or bias based on what i see in the photos.
His other more basic testing method that you see on that forum looks more apples to apples fair comparison.
docs.google.com/document/d/1cSzxgX9QSwvUyC2wql7uFOM1IYqEdjExvUkHLX_2nb8/edit The way it looks in Vlocicaptor's Doc is, he has very long 6m screws holding the test plate to the mast gong mast, with maybe 2" of drop-in before the screws reach the threads. So I'm assuming there is some tension stretch of these screws in his deflection measurements. From what he understand the Cedrus mast was bolted directly to the plate.
The measurement point should be from the fuselage for all three mast with appropriate adapters, not from the mast on one mast, and the fuselage on the other. Also the test plate should be attached to the fuselage (not the screws attaching the fuselage to the mast).
The test is not biased. The test method is reflective of the actual loading conditions that a foil mast experiences while being ridden. This is my last post on this, but a mast bolted to a wall with a weight hanging on the end is a completely flawed method of characterizing stiffness. I know that's how many brands test their masts, but based on engineering first principles, it is wrong.
To answer your question, you cannot change the stiffness of an alloy with temper or heat treatment. Tempers, heat treatments, and annealing procedures are primarily used to change strength and ductility, but will not affect the underlying modulus of elasticity (stiffness) of the alloy.
I am hoping to have first prototypes available later this [North American] summer. I'm I'm in final design of the profiles, detailing the adapter interface, and preparing to cut tooling (molds). I will be up front and share that the Evolution mast will retain the modularity of the current system with respect to mounts. I get a lot of requests for custom mounts, and it is still ultimately a stronger, more repairable, better for travel, and cheaper solution than integrated mounts. I can't think of a single benefit to the the integrated or monocoque designs, other than marketing. They are not any lighter, not any stronger, result in more expensive processes, and not repairable when compared to a properly designed and maintained bolted joint.
Thanks to all who contributed to the survey. Stay tuned to the site and feel free to subscribe to the newsletter for updates on becoming an Evolution Cedrus launch customer. Also for those interested in the design and engineering aspects of Project Cedrus, I shared the whole process on my blog. It's a lot more technical, and accurate, than a lot of the stuff being posted on forums these days. Here's an example of one I did on composites and solid mechanics:
projectcedrus.com/general/solid-mechanics-composites-101/