oogaboogachiefwalkingdeer
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Until they get a hole in them.
All materials fatigue if you apply enough stress.
The fatigue stress level for most materials is way lower than the level at which it will deform, so there is no way of knowing how much the material has weakened. Depending on the stress level, a material may last a few cycles, or millions before failure.
I had one batch go to 9 volumes (only 1 bottle broke) - I measured the gravity from another bottle to determine the carbonation level.
There are some 8 different formulas out there I've seen. But I use the Cooper's one that agrees with Beersmith2 so far; (OG-FG)/7.46 + .5= ABV%. So if your OG was 1.053 & your FG was 1.012, then, (1053-1012)/7.46 +.5=ABV% or 41/7.46 + .5 =ABV . 5.49597855227882 rounded off to 5.49 + .5 = 6.4% ABV.
Ok, but how do you get from ABV to carbonation level?
Brew on![]()
I think the highlighted statement conflicts with what most people who have learned about fatigue were taught. Do you have any support for that statement, and can you provide references? Would be nice if the references explained on a molecular level what leads to fatigue at very low stress levels.
Can you explain how you used gravity measurements to determine carb levels? It's not immediately clear to me how this would be done, and it sounds like it might be a useful method to know.
Yield stress is an engineering definition, conventionally set at some fixed amount of deviation from the linear portion of a stress/strain curve resulting from a standardized test. Plastic deformation starts as soon as stress is sufficient to cause any change in the microstructure of a solid material, even if the deformation is not detectable at a macroscopic level. These microstructural changes can occur at much lower stresses than the yield stress, as you have noted. It's the microstructural changes that accumulate over time, and multiple cycles, which eventually lead to fatigue and failure. I'm no expert on aluminum, so have no idea at what stress level microstructural changes can occur.No references, but if you look in any material handbook, you will find everything you need to know. Try googling Aerospace Materials Handbook, and research some steels or aluminum materials in it. The data should be there. I work in the Aerospace industry and material fatigue is a critical item. Just winging some numbers off the top of my head, but; cast aluminum yield strength is about 30 KSI. Yield is where it will permanently deform (plastic rather than elastic), but High Cycle Fatigue stress (the level you want to stay below to ensure infinite life) is around 12 KSI. These numbers are for high temperature applications, I don't know what room temperature capabilities are since I deal with hot parts.
...... And (before someone brings it up), there is actually no lower limit for aluminum for fatigue. It may take billions of cycles to fatigue, but aluminum will eventually fail at whatever level of stress you give it, if you cycle it enough times.
Ok, I get the general idea. Thanks.I bottled to 3 volumes. One bottle broke. I immediately put the rest in the fridge and set about consuming them as quickly as I could. I opened one of the beers, and let it go flat, and then took a gravity reading. It has been a while now, so my numbers may not be correct as I'm not looking them up, but I think I bottled at 1.016 (an Oatmeal Stout) and when measured sometime after bottling, it was something like 1.009. I calculated the difference in gravity to be about 6 volumes of CO2. Add that to the 3 I bottled at = 9 volumes.
^^^ this!
I had some bottles of stout blow up on me. It's enough to put the fear of God in you when you start handling the other bottles.
I bottled to 3 volumes. One bottle broke. I immediately put the rest in the fridge and set about consuming them as quickly as I could. I opened one of the beers, and let it go flat, and then took a gravity reading. It has been a while now, so my numbers may not be correct as I'm not looking them up, but I think I bottled at 1.016 (an Oatmeal Stout) and when measured sometime after bottling, it was something like 1.009. I calculated the difference in gravity to be about 6 volumes of CO2. Add that to the 3 I bottled at = 9 volumes.
1 gravity point drop will add about .51 volume of CO2 (last line under the title Remaining or Residual Effect).
I have seen other values (higher) for this. Is there a different formula that you are using? I've been taking this as gospel but really don't know if this is accurate or not.
I don't bottle as much anymore since I started kegging, but my original 22oz bombers from 5 years ago are still working fine and I've never had an issue.
In Europe they reuse bottles almost exclusively. You get a beer and the bottle is all scuffed up because they reuse instead of recycle, and based on how gnarly some of the bottles look we're talking hundreds of times most likely.
Thanks guys...I guess basic materials science hasn't changed much in the last 30 years![]()
Sorry about the self quote, but on further reflection, there is a way to tell if a bottle is strong enough to use safely. The method is a hydrostatic test, similar to what we have to have done to our CO2 cylinders periodically.Is there a reliable way to determine when they will break? No.![]()
10 Vco2 is a whole lot higher than the 3 1/2 Vco2 they say the average beer bottle can withstand. I didn't go higher than 2.8 Vco2 with my hefe & still got plenty of carbonation. Drove the head like a winter tornado.
The most recently bottled batch of beer I bottled was done with 1 full cup of agave nectar in about 4.5gallons of porter(I wanted to see what highly carbonated porter tastes like [it had an interesting mouthfeel and taste ]) It has more fermentables than a cup of table sugar. I'm a novice, first time bottling with glass bottles. No bottle bombs.![]()
Agave nectar is a syrup. The fermentable Part of Agave nectar is sugar. 1 cup of Agave nectar has less fermentables than 1 cup of sugar because it also has some water content. It probably has 25% less fermentables than sugar.