Snao G's
Gray E Fowler
gfowler at raytheon.com
Thu Jan 27 14:13:32 AKST 2005
Technically isn't a Rev avalanche snap just a negative level snap at the
speed at which you entered?
Or is it a SNAO?
Gray Fowler
Principal Chemical Engineer
Composites Engineering
Ed Deaver <divesplat at yahoo.com>
Sent by: discussion-request at nsrca.org
01/27/2005 05:07 PM
Please respond to discussion
To: discussion at nsrca.org
cc:
Subject: Re: Snao G's
So, if I am interpreting these numbers(realize only one day and flight)
correctly. Beings the straight and level pos snap at 100mph(not unusual
speed) was -13G's and the Rev avalance at approximately 95mph was -13G's,
then the forces are about the same.
So, if we can slow the rev avalanche down to 70mph then the G's would only
be -7.
This seems to go along with previous arguments that speed is the key.
My question is, if the G's on flat and level snaps are approximately the
same, with approx equal speeds, as the rev snap, then why hasn't FAI
pilots been breaking planes with the 1.5snapopp 4/8????
Before anyone says it, I have seen many of these 1.5 snaps flown with some
speed, so they weren't just puttputt into it.
Thanx Earl. Interesting stuff
ed
Earl Haury <ehaury at houston.rr.com> wrote:
FWIW, I took a quick look at some snap G's yesterday. Equipment was a
Quique YAK (140 size) fitted with an Eagle Tree Systems datalogger with G
sensor. I only gathered data from one flight - so take that into
consideration.
Flat and level pos snaps @ (nominally) 100mph = 13G, dropping the speed to
70mph = 7G. (A normal pull to vertical @ 100mph = 7G.)
An Avalanche with a neg snap at the top measured -5G @ 50mph.
A Rev Avalanche with a pos snap at the bottom measured 13G @ 95mph.
(Masters maneuver - intentionally flown fast.)
An Avalanche from the top (push - F05) with a neg snap and a half at the
bottom measured -14G @ 90mph.
(I normally measure around 5G on upline and downline snaps with my
Partner.)
All snaps were executed with rapid / high degree elevator lead and %
reduction of elevator during rotation.
I may look at this further as the mood strikes. As expected, controlling
speed into snaps is easier on your airplane. None of the observed loads
(in my opinion) should damage a well constructed aerobatic model (wouldn't
want to ride in it though).
Earl
-------------- next part --------------
An HTML attachment was scrubbed...
URL: http://lists.f3a.us/pipermail/nsrca-discussion/attachments/20050127/d47902a7/attachment.html
More information about the NSRCA-discussion
mailing list