Can we see the data on mahogany also for comparison?

That sounds like a book worth having.  Where can I buy a copy or is it
something from the FAA that I can download somewhere?

Brian Kraut
Engineering Alternatives, Inc.
www.engalt.com

-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
Behalf Of Mark Langford
Sent: Thursday, July 01, 2004 8:06 AM
To: KRnet
Subject: Re: RE: KR> spar skins


And having said that, here's one from Don Reid where he advocates running
the grain horizontal, rather than vertical.  I'd trust just about anything
Don says as gospel.
----------------------------------------------
List-Post: krnet@list.krnet.org
Date: Jul 20, 1999 8:27 AM

From: Donald Reid <donr...@erols.com>

Subject: Re: Grain direction.....who cares it's plywood...my turn at a
'STUPID' Question


Tim wrote:

> Like Aircraft Plywood is either 90 or 45 degrees, I assume this is how
> the ply's (3-7) are layered. So grain direction of the top sheet is of
> interest, but I wouldn't think the orintation is as critical in dealing
> with the Spar web as perhaps Aluminium .....

OK, here are some numbers.  Anyone who is interested can make up their
own mind.  All data are for birch plywood and taken from ANC-18, Design
of Wooden Aircraft Structures. (The thick pieces are included just to
show the effect with more plys)

thickness   # plys    parallel   perpendicular
0.125"         3       15.17         5.544
0.160"         5       21.46         11.47
0.410"         7       131.1         80.91

All plys are equal thickness.  The numbers are moment for fiber stress
at the proportional limit in units of inch-pounds per inch of width.

As to why the KR plans specify a vertical orientation, it is because Ken
Rand and Stu Robinson got it wrong.
-----------------------------------
Mark Langford, Huntsville, AL
N56ML at hiwaay.net
see KR2S project N56ML at http://home.hiwaay.net/~langford


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