Re: [RCSE] Re: 2M Rambles

2006-08-02 Thread Jeff Steifel
Actually Dave, this is a perfect place to go into detail. There has been 
so much dribble and little info that it is refreshing.


David Register wrote:

It's a little tough to go into too much more detail on RCSE. Also 
probably not of general interest to everyone on the list. Is this 
topic of sufficient interest to open a 2M forum on RCGroups where some 
more detailed numbers, graphs etc. can be posted. Or does such a forum 
already exist?


--
Jeff Steifel

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Re: [RCSE] Re: 2M Rambles

2006-08-02 Thread tony estep
 From: David Register [EMAIL PROTECTED]

Good luck with the girlfriends. In 
1963, Jimmy Soul had a #1 hit with some interesting advice along those 
lines.
=
Which said:

  If you wanna be happy for the rest of your life
  Never make a pretty women your wife
  Go for my personal point of view
  Get an ugly girl to marry you





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Re: [RCSE] Re: 2M Rambles

2006-08-02 Thread George Gillburg
 From: David Register <[EMAIL PROTECTED] />  Good luck with the girlfriends. In  1963, Jimmy Soul had
a #1 hit with some interesting advice along those  lines.  =  Which said:  
If you wanna be happy for the rest of your life  Never make a
pretty women your wife  Go for my personal point of view  Get an ugly girl to marry you  Just don't let
your wife know that's your philosophy if you want to go on living!George Gillburg Bakersfield, California 
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[RCSE] RE: 2M Rambles

2006-08-02 Thread Aradhana Singh Khalsa
Allegro broken with negative G's

Brent,
What was the mode of failure?
How would you build the wing differently if you wanted to survive a quick
and too deep dip into the bucket?

Aradhana Singh Khalsa
Espanola, NM

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RE: [RCSE] RE: 2M Rambles

2006-08-02 Thread Douglas, Brent
I really wouldn't change much beyond my launch technique.  If I do build
another, I would be a little more careful with my spar wrapping and
glueing of the center section, the centermost 6 inches in particular.  

I might consider adding a little more carbon in that same area if I had
some thin prepreg available, inside of the bottom spar?  It would just
take a little sanding down of those shear webs a bit.  

Again, it's pretty darn tough, but avoiding a deep dip is probably a
pretty good idea any way.

Good luck!
Brent
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[RCSE] Re: 2M Rambles

2006-08-01 Thread Lincoln Ross
Actually, I think, given the AG airfoils, optimum aspect ratio is 
probably a function of your vision. Given very good vision and very good 
skill with composites, optimum aspect ratio is probably upwards of 12, 
as in the original Agea 2M. More realistically, maybe a bit over 11. 
Wing loading shouldn't be an issue, given enough building skill, as 21 
oz. can be acheived. Maybe 25 oz. for all the other really good builders 
besides Mark. You can add ballast on windy days. Carbon tailbooms and 
some of the other more sophisticated building tricks keep the weight down.


Most of those old airfoils are now obsolete, aren't they? (I saw a new 
foil, a thicker one, on the yahoo xfoil group, which behaves just like a 
thinner AG, though)


In local contests, I end up competing against Mark. One of these days I 
want to see what happens if I have a glider almost as good as his is.



From: David Register wrote:
snip
snip

Beause of it's size, a 2M is not going to be able to roam as far 
or as high as an open class ship - it's simply harder to see at 
distance. So, like DLG, it's going to be more of a close-in ship. 
Consequently, it probably should tend to better minimum sink and max L/D 
rather than having great 'legs' for roaming all over the sky. This tends 
to drive the design towards lower aspect ratios. Due to the span limit, 
a high aspect ratio 2M may start to run into Re problems.


Carrying more wing area will allow a lower wing loading with modest 
attention to building techniques. This should also help with the launch 
as more area would help to carry the tow weight better.


The airfoils often used for 2M are not particularly well optimized for 
this class. If you run X-Foil snip


So a couple of suggestions;
- Look to lower aspect ratio designs. An evaluation discussed in RCSD a 
few years back suggests the 8 to 11 range is about right.snip
- Sort through the Drela sections, many of them are much better in the 
intermediate speed range than any of the sections commonly used for 2M,

snip
- Work a bit on keeping the weight in the 30oz range. A ballast box is 
great for the windy days but it's tough to add lightness.


snip

- Dave R


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[RCSE] Re: 2M Rambles

2006-08-01 Thread David Register

Daryl (and list),

Thank you for the comments on 2M design. Your input is extremely 
valuable as both a designer and competitor. The stability issue is well put.


Just to clarify aspect ratio a bit, some design work was done 2 years 
ago that suggests optimal AR for 2M is somewhere between 8 and about 11. 
The range and boundaries are 'soft' depending on the pilot's 
preferences. This was done on the basis of a fairly detailed polar 
analysis which uses UIUC airfoil data or X-Foil results, a modestly 
detailed description of the planform and some assumptions about 
parasitic drag and fuselage wetted area.


Why such a broad range? Well, once a design is set, decreasing AR 
increases wing area (and the associated tail volumes) which increases 
the weight (but reduces the wing loading), increases induced drag, 
reduces profile drag coefficients a bit due to Reynolds number, etc. 
etc. It's an interesting interplay but one has to consider that weight 
is not an arbitrary parameter but is tied to the planform once a general 
construction method is adopted.


The span loading issues that you mentioned are not addressed in this 
type of analysis. Nor are handling, turning, stability, etc. etc. So 
there's a lot more to the picture once the general planform parameters 
are established. Field experience and the pilot's preferences are the 
deciding factors.


The other thing that comes into play (for 2M and smaller) is the flow 
attachment on the airfoil. The Drela sections are just better designed 
that way than just about anything that preceded them. You can compare 
X-Foil with UIUC data for those sections where measurements have been 
made. The result is generally gratifying. Extending that analysis to the 
AG sections leads to the observation of separation bubbles in many of 
the popular sections used for 2M. The bubble generally appears at modest 
Cl values so the problem is not high drag at high Cl (low speeds) but in 
the intermediate speeds (cruise). Consequently, airfoil choice for 2M 
will be particularly sensitive in the mid-speed range (generally higher 
than max L/D - about the range where you want to scoot to cover ground). 
At these Cls, induced drag is not really an issue (AR is not terribly 
important at lower Cl). Profile drag is the big issue and the non-Drela 
sections are generally not great in this range. When you go to open 
class, the chords and speeds go up enough that the problem tends to go away.


Bottom line, there are a lot of trade-offs. Input from guys who have 
your level of field experience are invaluable to the design process. 
Polars look real good on paper but if all it does is run great in a 
straight line then it's not much use. However, a polar is a useful 
starting point and the calculations are generally supported by what 
little field data there is.


It's a little tough to go into too much more detail on RCSE. Also 
probably not of general interest to everyone on the list. Is this topic 
of sufficient interest to open a 2M forum on RCGroups where some more 
detailed numbers, graphs etc. can be posted. Or does such a forum 
already exist?


Thanks very much for the feedback Good luck with the girlfriends. In 
1963, Jimmy Soul had a #1 hit with some interesting advice along those 
lines.


- Dave R
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