[SPAM] Re: Snao G's
Ken Thompson III
mrandmrst at comcast.net
Fri Jan 28 16:59:05 AKST 2005
I'm repairing a fuse on a profile right now because of "managing my energy" too close to the ground.
Ken
----- Original Message -----
From: Cameron Smith
To: discussion at nsrca.org
Sent: Friday, January 28, 2005 8:05 PM
Subject: RE: [SPAM] Re: Snao G's
I look at it more as "Energy Management". I'm replacing wings on a large gasser from "Poor Energy Management" Dropped it to far with NO throttle & Pulled a Sharp Parachute and the Crack could be heard across the county.
-----Original Message-----
From: discussion-request at nsrca.org [mailto:discussion-request at nsrca.org] On Behalf Of Ken Thompson III
Sent: Friday, January 28, 2005 5:57 PM
To: discussion at nsrca.org
Subject: Re: [SPAM] Re: Snao G's
Walls I can see the stress, however I understand that the correct way to enter a wall is at 1/4 throttle or less. I'm not one of those big ego guys, so correct me if I'm wrong.
Parachutes are more of a controlled fall, from a partial wall up high, and Blenders begin from a stalled state. Of course when you slam the throttle to push the plane through the Blender, that could hurt a bunch.
Ken
----- Original Message -----
From: Ed Alt
To: discussion at nsrca.org
Sent: Friday, January 28, 2005 5:05 PM
Subject: [SPAM] Re: Snao G's
Yep, but the transition into it can be stressful. Stuff like Walls, Parachutes, Blenders, certain brands of Waterfalls put mucho strain in the airframe.
Ed
----- Original Message -----
From: Ken Thompson III
To: discussion at nsrca.org
Sent: Friday, January 28, 2005 4:16 PM
Subject: Re: Snao G's
Matt,
I could be wrong, but isn't 3D, by definition, done in a constant state of stall? Wouldn't that eliminate a lot of the high G's in the maneuvers? I wouldn't think the airframe would be in as stressed state, when the flying surface is depending on prop wash, not air speed, to do it's thing.
Ken
----- Original Message -----
From: Rcmaster199 at aol.com
To: discussion at nsrca.org
Sent: Friday, January 28, 2005 1:46 PM
Subject: Re: Snao G's
If this accelerometer is finding 13 G loads generated by a Pattern model snap, a relatively low amount really, I imagine that a 3D model set up for a full array of stunts has to be experiencing double that at least.
Earl could you do any 3D type maneuvers and measurements with the Yak?
Very informative discussion BTW, and may result in improved more efficient building technique, read-- lightest for the desired strength.
thanks
matt
In a message dated 1/28/2005 1:32:35 PM Eastern Standard Time, d.pappas at kodeos.com writes:
That's proof of stall!
If the G loading rises suddenly, and then holds or droops continuously during the roll, then it's probably an accelerated barrel.
If the profile is sudden rise, sudden drop to maybe 1/2, then onload, you have a real snap.
Yia,
Dean
Dean Pappas
Sr. Design Engineer
Kodeos Communications
111 Corporate Blvd.
South Plainfield, N.J. 07080
(908) 222-7817 phone
(908) 222-2392 fax
d.pappas at kodeos.com
-----Original Message-----
From: discussion-request at nsrca.org [mailto:discussion-request at nsrca.org]On Behalf Of Rcmaster199 at aol.com
Sent: Friday, January 28, 2005 11:45 AM
To: discussion at nsrca.org
Subject: Re: Snao G's
Good point. Once in the stall, the model should not see the same continued G load. Should drop dramatically. If the plane doesn't stall to begin with, different story.
Matt
In a message dated 1/28/2005 11:23:25 AM Eastern Standard Time, d.pappas at kodeos.com writes:
Let me add another two cents worth ...
Earl,
What is the sampling rate on your data logger?
Can you see if the maximum 13-Gs at 100 MPH was sustained for the entire half second or so that it took to complete the snap,
or was it a short spike (like 0.1 second) and then sustained at say half of that value, for the rest of the snap.
Of course, if the data logger samples once a second, we have almost no way of knowing.
Later,
Dean
-------------- next part --------------
An HTML attachment was scrubbed...
URL: http://lists.f3a.us/pipermail/nsrca-discussion/attachments/20050129/cad7795d/attachment.html
More information about the NSRCA-discussion
mailing list