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Green Building Bible, Fourth Edition
Green Building Bible, fourth edition (both books)
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  1.  
    We are building a living roof. on loadbearing straw walls.
    The (dead&live) load for the beams is 185kg per m2
    The span for the round larch beams is 4meters
    Round larch beams between 7" and 9'' diameter.
    They look the part but how do we prove it with numbers?
    •  
      CommentAuthorSteamyTea
    • CommentTimeNov 2nd 2015 edited
     
  2.  
    Ben Law's book has some of the calcs his SE did for his roundwood building.
    •  
      CommentAuthorfostertom
    • CommentTimeNov 2nd 2015
     
    As Nick says - roundwood, which hasn't had all its outer, most stressed fibres shredded by machining, has considerably higher stress capacity than the standard figures for that timber species. Tree trunks/branches are amazingly strong.
    • CommentAuthorTimber
    • CommentTimeNov 2nd 2015
     
    Well the official way would be to get them visually graded to the softwood rules and then treat the cross section as square (losing the rounded bits). Calc as normal.
    •  
      CommentAuthorSteamyTea
    • CommentTimeNov 2nd 2015 edited
     
    Posted By: Timbertreat the cross section as square (losing the rounded bits). Calc as normal.
    Makes sense to me. Thee will only be a small difference in strength. Be different if it was hollow or being used as a shaft to transmit power.
    • CommentAuthormike7
    • CommentTimeNov 2nd 2015 edited
     
    <blockquote><cite>Posted By: SteamyTea</cite><blockquote><cite>Posted By: Timber</cite>treat the cross section as square (losing the rounded bits). Calc as normal.</blockquote>Makes sense to me. There will only be a small difference in strength. Be different if it was hollow or being used as a shaft to transmit power.</blockquote>

    The section modulus for a round log is (pi*r^3)/4 or 0.785r^3.
    Trim the log square and the modulus drops to (2.82*r^3)/6 which is 0.47 r^3
    The optimum rectangular shape is about 1.15r wide and 1.64 r high, giving 0.513 so that's lost a third of the round pole strength. Surprising eh?
    •  
      CommentAuthorfostertom
    • CommentTimeNov 2nd 2015
     
    An engineer would have the formula for round at his fingertips - I did once but have forgotten - it's easy.
    • CommentAuthormike7
    • CommentTimeNov 2nd 2015
     
    The max bending moment is wl^2/8 or 480*16/8 = 960kg.m
    Max stress is that divided by the section modulus which makes it about 250,000 kg/m^2
    Larch has a working tensile strength of about 70,000 kg/m^2 so you’d need at least 4 logs per metre.

    Max shear load is 480*2 = 960 kg/m
    Cross section area of 4 logs is 4*pi *0.09^2 or about 0.102 m^2
    Max shear stress is 960/.102 = 9400kg/m^ which is well below working shear strength of larch of about 80,000kg/m^2

    About.. you might want to check this, figures used for larch etc.
    •  
      CommentAuthordjh
    • CommentTimeNov 3rd 2015
     
    Posted By: Carol hunterThey look the part but how do we prove it with numbers?

    If you need to prove it, do you need to get an engineer to sign it off?
    • CommentAuthorEd Davies
    • CommentTimeNov 3rd 2015
     
    At one point I was interested in using Douglas fir for my posts and beams but was put off by the fact that it wasn't structurally graded. I know of some houses which have been built with it (near Loch Eribol, from the mill I was talking to) but when I asked the timber guy about that he didn't know how it was approved.

    Is there just some default strength which can be assumed for non-graded timber? Per species?

    Or can you just load test it? Using what safety factor? Every log?
    • CommentAuthorTimber
    • CommentTimeNov 3rd 2015
     
    No there is no default strength for non-graded timber. If it is not graded, then it has 'no known strength'.

    Any qualified visual strength grader can grade it!
    •  
      CommentAuthorSteamyTea
    • CommentTimeNov 3rd 2015
     
    Is fatigue ever taken into account with timber structures?

    Not often the maximum load on a house is reached, but there are many small loads, over many decades.
    • CommentAuthorTimber
    • CommentTimeNov 4th 2015 edited
     
    I am not sure about fatigue or 'work hardening', I am not sure that timber does fatigue as long as it is only loaded within its elastic limits. There considerations for creep as timber does creep over time.

    There are all sorts of 'factors' added into the strength calculations, I know one of them is creep, if fatigue is an issue then I am sure that an appropriate safety factor would be present.

    It is also worth remembering that there are only certain timber species where the original strength testing has been done. There are quite a few species that cannot be structurally graded - not because they are not capable of, its just that there is no know strength data for them, nobody has got round to testing it!
    •  
      CommentAuthordjh
    • CommentTimeNov 4th 2015
     
    I believe timber is generally believed to have much better fatigue properties than other, manufactured materials. That is one of its attractions in boat and aircraft building (strength for weight being the other great advantage).

    Google brings up some interesting points; according to:

    http://link.springer.com/article/10.1007%2FBF02265220

    "The extreme lack of a satisfactory data base and the persistent neglect of fatigue characteristics in wood material design is emphasized." December 1980

    However http://www.byg.dtu.dk/-/media/Institutter/Byg/publikationer/byg_rapporter/byg_r038.ashx has:

    "Wood fatigue is of interest in regular fatigue loaded structures such as wood bridges but
    wood fatigue also covers low cycle fatigue encountered in ordinary structures. The study
    concentrates entirely on fatigue in tension perpendicular to the grain as this strength
    parameter often is strength limiter in critical details." 2002

    and http://eu.wiley.com/WileyCDA/WileyTitle/productCd-0471487082.html looks like it might be the dogs danglies if you have the dosh. Though there might have been some advance in the last decade or so.
    •  
      CommentAuthorfostertom
    • CommentTimeNov 4th 2015
     
    Doesn't fatigue happen when there's constant load reversal, like a Comet's wing? Or bending a bit of wire to and fro to break it? Building elements suffer v litle load reversal - except airtight membranes!
    •  
      CommentAuthorSteamyTea
    • CommentTimeNov 4th 2015 edited
     
    From what I understand, fatigue is cyclical loading, usually below the elastic limit.
    It is also affected by temperature, and with semi porous materials, probably moisture/humidity levels.

    It is hard to fatigue a car tyre, but easy to do a bit of mild steel.
    I suppose it is not much of a problem as we would have heard about it. But I have been in some creaky boats that have got me worried in the past.

    Moving on from that a bit. I think timber fails in a more 'gentle' way than masonry and steel.
    I know that some of the composite chassis cars I was involved with has some serious problems. Got around some of the problems by laminating in composite tubes as they failed in a more predicable way.
    • CommentAuthorchuckey
    • CommentTimeNov 5th 2015
     
    I removed a 14" by 4" purlin from a Victorian pig sty, I compared its deflection with a C24 9" X 2" modern joist and I found that its deflection over 10' with my weight on it was 3mm, against < .5mm for the modern joist. When I cut it up into mantle piece lengths, the wood worm had not penetrated by more then 6mm around the edges.
    I am still confused by these measurements and can not relate them to any known timber data, as timber is not thought to age. Did they use a specially weak timer? :-)
    Frank
    •  
      CommentAuthorfostertom
    • CommentTimeNov 5th 2015
     
    Ah that's pig fumes does that
    • CommentAuthorgyrogear
    • CommentTimeNov 5th 2015
     
    Posted By: fostertomDoesn't fatigue happen when there's constant load reversal, like a Comet's wing? Or bending a bit of wire to and fro to break it? Building elements suffer v litle load reversal - except airtight membranes!


    +1 for the constant load-reversal !

    There was actually nothing wrong with the Comet wing - it was the windows !
    They had square-cut corners, and failed due to metal fatigue.

    The constant load-reversal comes from repeated pressurizing and depressurizing of the cabin, stretching (stressing) the structure.

    Only pointing this out for one reason: the exact same phenomenon (of load-reversal) occurs on windows...

    In particular, on metal window frames (read french windows, patio doors etc.) namely from wind pressure (whence requirement for wind-loading certification...)(air wind and water-tightness tests).

    ref (http://www.consumerschoice.ca/windows/window-classification/)

    In particular, if the corners are not correctly jointed, or are correctly jointed (at the factory) but said window units are not correctly transported (trucked without use of braces) or are stressed during emplacement (craning, bad handling...), then they WILL leak, even if it takes a while for the repeated action of the wind, pushing then releasing the window...

    They might leak air, or water, or both, but they *will* leak...

    gg
    •  
      CommentAuthorfostertom
    • CommentTimeNov 5th 2015
     
    Posted By: gyrogearthe exact same phenomenon (of load-reversal) occurs on windows...
    As I said, it occurs even more significantly, for same wind-buffet reasons, on airtight (or any) membranes/tape. Explains a lot about their notorious failure rate.
  3.  
    Thanks for all your ideas. Really.

    In repy to djh's question. So far we have provided all construction drawings and calculations from our own hands referencing the many sources available to substantiate our plans.The inspectors seem satisfied with our diligence and knowledge. Therefore if we can crack it we won't need an engineer.

    But the question we have raised is stretching our boundaries. The algebraic formula's looking quite esoteric. We'd like to be satisfied ourselves that what "looks the part" does the job.
    •  
      CommentAuthorSteamyTea
    • CommentTimeNov 7th 2015 edited
     
    Posted By: Carol hunterThe algebraic formula's looking quite esoteric
    It does look it, but all it is saying is, how much does it move when I put a load on it, why you end up with that odd looking m^4 unit.
    All that is saying is for a bit of material with dimensions m x m x m (which is m^3), how many m's does it move when loaded, so it becomes m x m x m x m (m^4).
    Or just jump on a bit and see if it feel strong enough.
  4.  
    Dont forget snow loading. Of course if you're in the Sahara, it may not be required. A foot of snow can add a LOT to your dead load.
    Just saying....
    •  
      CommentAuthorfostertom
    • CommentTimeNov 7th 2015
     
    In fact it totally dominates - no such thing as a 'lightweight' structure as far as calcs concerned!
  5.  
    <blockquote><cite>Posted By: mike7</cite>The max bending moment is wl^2/8 or 480*16/8 = 960kg.m
    Max stress is that divided by the section modulus which makes it about 250,000 kg/m^2
    Larch has a working tensile strength of about 70,000 kg/m^2 so you’d need at least 4 logs per metre.

    Max shear load is 480*2 = 960 kg/m
    Cross section area of 4 logs is 4*pi *0.09^2 or about 0.102 m^2
    Max shear stress is 960/.102 = 9400kg/m^ which is well below working shear strength of larch of about 80,000kg/m^2

    About.. you might want to check this, figures used for larch etc.</blockquote>
    • CommentAuthormike7
    • CommentTimeNov 9th 2015 edited
     
    Posted By: Carol hunter
    Posted By: mike7
    About.. you might want to check this, figures used for larch etc.


    Erblushmumble bit of an error here - correct figure for tensile strength is more like 500,000kg/m^2 or as it might be given now 5mPa.
    Assuming no other errors that'd mean 1 log per 2m, which seems like not a lot.

    I calculated the roof beam section once for a shed down my garden. It didn't break, but it did sag quite a lot
    • CommentAuthormike7
    • CommentTimeNov 9th 2015 edited
     
    Just typed in how to calc the sag and system deleted it rather than posting it. GRRRRRRR. Some sort of timeout I imagine.
    Unvarnished, the formula for sag at centre is 0.013 w .L^4 /E . I
    E is elasticity of 9.10^5 kg/m^2, I is section moment of pi/64 . d^4

    Flog through that and you might get deflection is 13p mm where p is the log pitch in metres
  6.  
    Hi Mike7,

    Tried to reply to your original post last night, but a similar gremlin deleted the post... Think I just took too long writing it, so here goes again!

    Thanks so much for these figures, but I think we need a dummy’s guide, as tried to work through them yesterday and there was lots that we just couldn’t understand, not having done any calculations like this before. Hope you don’t mind, but you may need to hold our hands! These might sound like silly questions:

    What does wl mean?

    What exactly is max stress? 250,000kg/m^2 seems a lot when our total load (including snow!) is only 185kg/m^2.

    Again (at the risk of sounding simple!), 500,000kg/m^2 seems like a very big number- can you please explain tensile strength? The total load of the materials above the beams is 18,053kg.

    Is the shear load figure the load that can be applied before shearing occurs?

    How did you arrive at the figure of one beam per 2m? Or beams are actually about 1.4m apart.

    Is ‘sag’ the same as deflection?

    Also, I don’t know if this will have any bearing on how you’re thinking about it, but thought a bit of extra background on the structure might be handy, as our roof isn’t a conventional one! The single-storey house is only 8m x 4m internal, with walls 0.5m thick. We have 7 beams in total, 2 sitting on top of the 5m walls, and 5 spanning the gap. The beams are equidistant and are sitting on composite posts creating a 10 degree pitch. Some of the beams had a slight curve in them, so we placed them with a high point in the middle to help balance out deflection.

    Any more help would be much appreciated!

    Many thanks :-)
    • CommentAuthormike7
    • CommentTimeNov 9th 2015 edited
     
    These webpages should help you more competently than I can:-

    http://www.engineeringtoolbox.com/beam-stress-deflection-d_1312.html

    http://www.roymech.co.uk/Useful_Tables/Timber/Timber_design.html#Service

    Looking at it I discovered more errors in my posts. I made these posts hoping to be helpful but also to remind my aging grey matter how to do what I used to be able to years ago. Unfortunately my aging grey matter now seems very prone to clerical errors, and so my advice would be to ignore them.
   
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