VansAirForceForums  
Home > VansAirForceForums

- POSTING RULES
- Donate yearly (please).
- Advertise in here!

- Today's Posts | Insert Pics


Go Back   VAF Forums > Model Specific > RV-12/RV-12iS
Register FAQ Members List Calendar Today's Posts

Reply
 
Thread Tools Search this Thread Display Modes
  #11  
Old 02-05-2017, 02:36 PM
ILikePike ILikePike is offline
 
Join Date: Jan 2011
Location: Eatonton, GA
Posts: 215
Default

DonFromTX, I did notice that your external stiffeners were riveted to the formers. This may help keep any cracks from forming???

Jon, I don't think my roar is from the cowl. I built up the edge with micro to make a 3/4 strip for the felt to sit flat on the top skin. It adds stiffness and seals very well.
__________________
Jeff Green
2016 RV-8 #82985
1968 E33C Aerobatic Bonanza
Pleased to donate Dec 2019
Reply With Quote
  #12  
Old 02-06-2017, 06:43 AM
BillL BillL is offline
 
Join Date: Sep 2007
Location: Central IL
Posts: 5,514
Default stiffener alternative - rotate 90 deg

Quote:
Originally Posted by sf3543 View Post
To keep it from causing cracks at the ends of the added angles, the angles should be attached to the two bulkheads at each end. A joggle to lap over the flange at an existing rivet or a 90 bend and riveted to the bulkhead if the flange is on the other side of your stiffener.
Quote:
Originally Posted by ILikePike View Post
DonFromTX, I did notice that your external stiffeners were riveted to the formers. This may help keep any cracks from forming???
There are a couple of loadings that cause cracks. One is the pressure loads from the skin which loads the stiffener, well, like a beam. That loading will concentrate on the skin with no stiffening at the end if not attached to the bulkhead. However on that part of the fuse, there are longitudinal forces stretching the skin between the bulkheads, and attaching to the bulkhead will do nothing for that. There is a lot of skin there, and if the "stiffener" is the same thickness then is is likely of little consequence but would concentrate that stiffer effect at the last rivet.

I avoided (-7) the lengthwise stiffening all together by forming a couple of .025 bulkhead-like lateral stiffeners and did not rivet them into the J channel they do attache to the skin overlap rivet line. They were formed over a buck made to the floor contour, standard flange and just under an inch tall. Three rivets with 3M weather weld - bonding to the floor. Prior to stiffeners, a feather light touch was all that was needed to initiate the oil can and with some down force on the tail it self initiated easily.

YMMV
__________________
Bill

RV-7
Lord Kelvin:
“I often say that when you can measure what you are speaking about,
and express it in numbers, you know something about it; but when you
cannot measure it, when you cannot express it in numbers, your knowledge
is of a meager and unsatisfactory kind.”
Reply With Quote
Reply



Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT -6. The time now is 04:05 PM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.