[RCSE] 2 meter and how it fits

2005-02-18 Thread Mike Stump
After lurking and reading the many comments re 2 meter at the NATS I 
figured it was time to submit my dime's worth..

Let's first look at how 2 meter differs from the only other TD class 
(unlimited).. Because there really are just 2 true model classes for 
soaring for the major TD classes at the NATS (based on wing-span of 
course)... Again, these are based on wing-span, just like our full-scale 
counterparts...

With the span limited to 2-meters as compared to unlimited planes we're 
working with the following span-based performance limitations

less aspect ratio, limited visual profile at a distance, shorter glide 
ratio,  generally higher wing loadings.

This creates an entirely different flying environment and potential 
strategy for dealing with a given task. As I've read from a couple 
contributors, the limitation of size makes the 2 meter a bit more difficult 
to achieve a given task at times. This is something that makes 2 meter 
unique as compared to unl. span planes, whether full-house or limited 
function (the RES class)...

One of the tenets laid out by Dan Pruss was that a soaring champion should 
show abilities in multiple disciplines and various aspects of Soaring.. 
Within the practical realm of the Soaring NATS in which we deal, 2 Meter is 
the other discipline.. There is no other.

If you take a look at our recent NATS Champs, the Dan Pruss Award has 
required excellence in both disciplines.. This should not change..

There have been other numerous comments referring to 2 meter as an entry 
level class. While it's true that many of us started with 2 meter planes 
like the Gentle Lady, in fact they were RES planes. At the NATS level, the 
competitive end of 2 meter can't be viewed as such.

The entry level category (and throw-back class) is RES. It was before it 
became a rule-book category.

Those that were involved in the early years of the present NATS structure 
might remember that we added RES/NOS at the end of the NATS week as sort of 
a laid back way to finish the week, replacing Sportsman's F3B (which 
occasionally was anything but). It was an easy day of relaxed competition 
before we all went home.

If we want more RES rounds, maybe we should fly just RES on the last day. 
There is a fair amount of cross-over/redundancy on RES/NOS day anyway. 
Maybe another event (like one of the Woody Majors) could host a Nostalgia 
Championship for those so inclined.

my dimes worth
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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Oleg Golovidov
  
Yes, but also  what's happening (for a fixed wing span) is a  trade off 
between wing loading and induced drag. Re (at least for DLG chords and  up) is 
a variable but not the dominant one.

As you increase aspect ratio (reduce chord for a fixed wing span),  induced 
drag goes down but wing loading goes up. The wing loading will  eventually 
degrade your sink rate more than the aspect ratio improves it.  Although the 
wing 
weight scales with area, the total weight does not (fuselage,  tail surfaces, 
ancillary equipment). Re will hurt here as well (both Cd and Cl)  but it's 
primarily the loading (except perhaps at very small chords).

On  the other end, lower aspect ratio gives a lower wing loading but 
increased  induced drag (Cl^2/(Pi * AR).

Dave, you should know that for a fixed wing span, you need to be talking about 
total drag, not a drag coefficient, because you are changing the wing area when 
you change the aspect ratio. Total induced drag depends on the span only (for a 
constant weight and flight speed). Changing aspect ratio with a fixed span does 
not affect induced drag (if we ignore that the weight of the structure 
changes). 
Induced drag is proportional to the span loading squared (the formula below is 
obtained by manipulating the one above Cdi=Cl^2/(Pi*AR)):

D = (W/L)^2/(Pi*q), where q = rho*V^2/2

Therefore with a fixed span, you can easily find a wing area that gives you the 
best L/D ratio (parasite drag = induced drag). But that maybe still not the 
best 
design depending on your objectives. The main trade-off variables are min 
flight 
speed (affects turn radius), best L/D ratio, and high speed performance, all of 
which are directly affected by the wing area. Obviously, reducing the weight 
and 
parasite (fuselage, tail) drag allows to improve all of the criteria because 
the 
optimum wing area becomes smaller.

Comments and corrections are most welcome.
Regards,
Oleg.

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[RCSE] Fw: f3j team wanted

2005-02-18 Thread Richard L Bothell


- Original Message -
From: Rick Bothell
Sent: Thursday, February 17, 2005 10:57 AM
To: [EMAIL PROTECTED]
Subject: f3j team wanted

Wanted:  To either form a 4 person F3J team or to join a team that is short a 
flyer to fly in the Soaring in the Rockies on May 28,29.  Denver, Colorado 
and/or the NATS .Good chance I can find one team mate here in Arizona.  I 
have equipment, knowledge, and can tow.  Placed 5th in 2003 F3J Soaring in the 
Rockies.   Please e-mail me if you are interested.   Thanks, Rick Bothell,   
Prescott Valley, AZ


[RCSE] Re: Hey Melborne Australia, I'll be there Friday morning!

2005-02-18 Thread AntonL

Hi Gordy,

Just happened to see your post about being in Melbourne. What sort of
soaring were you interested in? How long are you here for? Did you
bring any planes?? :)

I'm mostly into slope soaring but I don't know if I can get out
anywhere this weekend...  Nevertheless, you're welcome to get in touch
if you'd like some info about flying sites etc. Email: anton AT
primarykey DOT net DOT au or phone: 9593 9550 (preferably after 10am if
calling on the weekend! :p ).

I'll give you the main flat-field address for soaring:

Directions from VARMS site guide:

VARMS (Victorian Association of Radio Model Soaring)
Briggs Field
Wantirna South
Melways Map 72, C2-D2
Opposite Jenkins' Orchard, with red, green  yellow apple sign. Gravel
driveway South off High Street Road, enter through gate and proceed down
track to car park left of hut.

There will most likely be guys flying there on Sat and Sun if the
weather is not too wet.

Enjoy your stay!

Anton


-- 
AntonL

AntonL's Profile: 
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[RCSE] ATTN: Sharon 3.7 x-tail owners, need input

2005-02-18 Thread Stan Myers
Had all but decided on Tempest when the water got muddy. Someone(read 
Edgar Soaring Junkie) suggested I consider the Sharon.   So, I'm 
asking for input. Probably the main criteria I have is that it be able 
to hi-start.  I do not have a winch readily available to me(and the club 
winch has seen better days). I am able to get 23#'s of pull out of my hi 
start. Which was adequate for my Artemis 5mph +, but really iffy for 1-3 
mph.

That aside, does it require constant attention with the sticks?  I'm a 
Sunday Flyer and I am looking for 'relaxed' flying.  I have some open 
class flying experience. I have a Sun 3.2m electric powered by Hacker 
50 that I am able to handle, but never really got comfortable with the 
Artemis V tail.

Any and all suggestions would be appreciate.
Yes I'm the same guy who asked about the Tempest last week. Appreciate 
the band width.

Stan
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RE: [RCSE] Re: Hey Melborne Australia, I'll be there Friday morning!

2005-02-18 Thread Dave Brombaugh
 Did you bring any planes??

Are you kidding?  Gordy never goes anywhere without an airplane; he will
likely be buried with his Pike Superior. :)

-Original Message-
From: AntonL [mailto:[EMAIL PROTECTED] 
Sent: Friday, February 18, 2005 05:33
To: soaring@airage.com
Subject: [RCSE] Re: Hey Melborne Australia, I'll be there Friday
morning!


Hi Gordy,

Just happened to see your post about being in Melbourne. What sort of
soaring were you interested in? How long are you here for? Did you
bring any planes?? :)

I'm mostly into slope soaring but I don't know if I can get out
anywhere this weekend...  Nevertheless, you're welcome to get in touch
if you'd like some info about flying sites etc. Email: anton AT
primarykey DOT net DOT au or phone: 9593 9550 (preferably after 10am if
calling on the weekend! :p ).

I'll give you the main flat-field address for soaring:

Directions from VARMS site guide:

VARMS (Victorian Association of Radio Model Soaring)
Briggs Field
Wantirna South
Melways Map 72, C2-D2
Opposite Jenkins' Orchard, with red, green  yellow apple sign. Gravel
driveway South off High Street Road, enter through gate and proceed down
track to car park left of hut.

There will most likely be guys flying there on Sat and Sun if the
weather is not too wet.

Enjoy your stay!

Anton


-- 
AntonL

AntonL's Profile:
http://www.rcgroups.com/forums/member.php?action=getinfouserid=28609
View this thread:
http://www.rcgroups.com/forums/showthread.php?threadid=337195

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[RCSE] Best 2m electric?

2005-02-18 Thread Soareyes



Hi guys,
I haven't been flying as much as I use to, but when I do, I find my little 
1.5m Koleos electric is the planeI grab. Its small and lightenough I 
can fly from the small field behind my house where my larger electrics aren't 
comfortable. The Koleos is getting pretty worn out, and I am looking for 
something slightly bigger, around 2m. What's available as an electric in this 
size? Anything with AVA-type construction (very light)and 
rudder/elevator/spoiler? TIA
Stan Sadorf



RE: [RCSE] Best 2m electric?

2005-02-18 Thread Aradhana Singh Khalsa



Wind Dancer!
http://www.polecataero.com/

Based on the Allegro E-Lite. RES, built up, 
lightweight.

A few guys were flying thesefor Spd 
400 during the 2004 ESWC in New Mexico.Two of themplacedsecond 
and third.

Aradhana Singh Khalsa
Registrar
2005 F5J Electric Soaring 
Challenge
October 14-16th, 2005
http://www.soarabq.org


[RCSE] Pivoting laser level

2005-02-18 Thread Murrill Barry Maj 107ACS/DO
Someone recently was looking for a laser that would project a crosshairs at
the floor. I don't remember who it was (sorry) but I came across a Bushnell
PivotPoint Laser Level # 82897 at the local Fry's grocery store that fits
the bill. It will project a dot, line , or crosshairs anywhere from straight
up to straight down. It was on sale for $14.97. Hope this helps.

Barry Murrill
Phoenix, AZ
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Re: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input

2005-02-18 Thread mpodder
Hi Stan
For me the best all around ship is the new Escape Lt. from Aero Model 
http://www.aero-model.com/ProductDe...x?productID=429 It only weighs 68 oz 
(it will go up on a good hi-start or a weak winch with no problem) but can 
carry, safely, up to 24 oz. of ballast. So you have a plane that is light 
enough for the deadest days and strong enough to carry 9 or 24 oz. (this is 
the 2 ballast bar set available from Aero Model for $49.00) of ballast for 
the windiest days. I love the plane and have 2. You can see them and the 
slight mods that I made to them on rcgroups/thermal/Escape Lt. or use the 
link below. http://www.rcgroups.com/forums/show...690#post3174690

Maurice
- Original Message - 
From: Stan Myers [EMAIL PROTECTED]
To: Soaring Digest soaring@airage.com
Sent: Friday, February 18, 2005 8:26 AM
Subject: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input


Had all but decided on Tempest when the water got muddy. Someone(read 
Edgar Soaring Junkie) suggested I consider the Sharon.   So, I'm asking 
for input. Probably the main criteria I have is that it be able to 
hi-start.  I do not have a winch readily available to me(and the club 
winch has seen better days). I am able to get 23#'s of pull out of my hi 
start. Which was adequate for my Artemis 5mph +, but really iffy for 1-3 
mph.

That aside, does it require constant attention with the sticks?  I'm a 
Sunday Flyer and I am looking for 'relaxed' flying.  I have some open 
class flying experience. I have a Sun 3.2m electric powered by Hacker 50 
that I am able to handle, but never really got comfortable with the 
Artemis V tail.

Any and all suggestions would be appreciate.
Yes I'm the same guy who asked about the Tempest last week. Appreciate the 
band width.

Stan
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and unsubscribe requests to [EMAIL PROTECTED]  Please note 
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AOL are generally NOT in text format


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RE: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input

2005-02-18 Thread Lex Mierop
Stan,

I picked up this very plane (incidentally pushed by the very same
person.  Edgar gets around ;-) last November.  It's big, but that also means
it's heavy. If you high-start is iffy for the Artemis, it's not going to be
enough for the Sharon. If you go with the Sharon, either upgrade the
High-start, or volunteer to take over winch maintenance.

That said, the Sharon is a great flyer.  First flight I set it up
per factory recommendations (except the tow hook is too far forward).
Launch climb was aggressive  it required 0 trim adjustments. (gotta love
the repeatability of molded planes)  Nice balance of stability vs. showing
air. I'm sure you could tweak the CG if you want more stability.

-l

-Original Message-
From: Stan Myers [mailto:[EMAIL PROTECTED]
Sent: Friday, February 18, 2005 8:27 AM
To: Soaring Digest
Subject: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input


Had all but decided on Tempest when the water got muddy. Someone(read 
Edgar Soaring Junkie) suggested I consider the Sharon.   So, I'm 
asking for input. Probably the main criteria I have is that it be able 
to hi-start.  I do not have a winch readily available to me(and the club 
winch has seen better days). I am able to get 23#'s of pull out of my hi 
start. Which was adequate for my Artemis 5mph +, but really iffy for 1-3 
mph.

That aside, does it require constant attention with the sticks?  I'm a 
Sunday Flyer and I am looking for 'relaxed' flying.  I have some open 
class flying experience. I have a Sun 3.2m electric powered by Hacker 
50 that I am able to handle, but never really got comfortable with the 
Artemis V tail.

Any and all suggestions would be appreciate.

Yes I'm the same guy who asked about the Tempest last week. Appreciate 
the band width.

Stan

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unsubscribe requests to [EMAIL PROTECTED]  Please note that
subscribe and unsubscribe messages must be sent in text only format with
MIME turned off.  Email sent from web based email such as Hotmail and AOL
are generally NOT in text format
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Re: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input

2005-02-18 Thread mpodder
Sorry the links didn't work.  Here are corrected ones.
http://www.aero-model.com/ProductDetails.aspx?productID=429
http://www.rcgroups.com/forums/showthread.php?p=3174690#post3174690
- Original Message - 
From: Stan Myers [EMAIL PROTECTED]
To: Soaring Digest soaring@airage.com
Sent: Friday, February 18, 2005 8:26 AM
Subject: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input


Had all but decided on Tempest when the water got muddy. Someone(read 
Edgar Soaring Junkie) suggested I consider the Sharon.   So, I'm asking 
for input. Probably the main criteria I have is that it be able to 
hi-start.  I do not have a winch readily available to me(and the club 
winch has seen better days). I am able to get 23#'s of pull out of my hi 
start. Which was adequate for my Artemis 5mph +, but really iffy for 1-3 
mph.

That aside, does it require constant attention with the sticks?  I'm a 
Sunday Flyer and I am looking for 'relaxed' flying.  I have some open 
class flying experience. I have a Sun 3.2m electric powered by Hacker 50 
that I am able to handle, but never really got comfortable with the 
Artemis V tail.

Any and all suggestions would be appreciate.
Yes I'm the same guy who asked about the Tempest last week. Appreciate the 
band width.

Stan
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and unsubscribe requests to [EMAIL PROTECTED]  Please note 
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Re: [RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Thomas Koszuta
There was a study done by Blaine K. Beron-Rawdon of Envision Design, at 
least a few years ago.  I will post this to news:rec.models.rc.soaring  for 
your perusal.  The study spanned several wingpans and aspect ratios and has 
a document that summarizes the results.

E-mail if you need a copy directly.
Tom Koszuta
Western New York Sailplane and Electric Flyers
Buffalo, NY
- Original Message - 
From: [EMAIL PROTECTED]
To: [EMAIL PROTECTED]; Soaring@airage.com
Sent: Friday, February 18, 2005 12:59 PM
Subject: [RCSE] Re: Optimum aspect ratio - induced drag and span


So which term dominates is not completely clear without running  through a
bunch of numbers and making some estimates of weights, planforms, etc. 
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Re: [RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Rick Van Clief
Dave,
A while back I sent you some comments on my admittedly amateurish approach 
to 2M based on Martin Simons work back in the 80's.  AR's are around 6 
-  max chord around 16,  min = around 8  Would you care to discuss how 
this approach fits into your current discussion?

RVC

At 12:59 PM 2/18/2005 -0500, you wrote:
In a message dated 2/18/2005 9:11:49 AM Central Standard Time,
Soaring@airage.com writes:
Changing aspect ratio with a fixed span does not  affect induced drag (if we
ignore that the weight of the structure changes).  Induced drag is
proportional to the span loading squared (the formula below is  obtained 
by manipulating
the one above Cdi=Cl^2/(Pi*AR)):

D =  (W/L)^2/(Pi*q), where q = rho*V^2/2

Oleg,
This does not seem to be dimensionally  correct.
In english units D is in lbs., V is in ft/sec, W/L is in  lb/ft^2, and rho
(density) is in slugs/ft^3 (gotta love those english density  units!).
Converting from density to weight (density * g ) gives the left side 
in  lbs and the
right side in lbs/ft^2.

I believe the missing term is the  average chord (Cavg^2).
Absent that, I'll generally be in agreement with  your comments with a few
caveats:
Assuming the following is correct (my  derivation of the same manipulation
you've done using the equations Lift = q *  Cl * A,Drag = q * Cd * A,
where A is the wing  area):
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[RCSE] Anyone have an F3B model for sale? Need practice ship...

2005-02-18 Thread Adam Till \(Cal\)
Hi folks,

Before I get lured away by a friend wanting to split shipping on some
scale models, does anyone have any F3B models for sale that would make
good practice ships? There's a group of us who have decided to learn to
fly the tasks properly this season, and from what I've been learning my
Erasers might not cut it.

Then again, I could solve the problem by just doing both :)

Cheers,
Adam

Adam Till 
Mechanical Engineer
403-270-9200 (ext 154) 
403-270-0399 (Fax) 
UMA Engineering Ltd. 
2540 Kensington Road NW 
Calgary AB, Canada T2N 3S3 

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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Oleg Golovidov

This does not seem to be dimensionally  correct.

In english units D is in lbs., V is in ft/sec, W/L is in  lb/ft^2, and rho 
(density) is in slugs/ft^3 (gotta love those english density  units!). 
Converting from density to weight (density * g ) gives the left side in  lbs 
and the 
right side in lbs/ft^2.

I believe the missing term is the  average chord (Cavg^2).

I have to admit that I am not well versed in English units (and probably will 
never be), but here is the dimensionality check in SI units for you:

D(N) = [ W(N)/L(m) ]^2 / [Pi*q(kg/m*s^2)],

(note, that W = m*g (N = kg*m/s^2)), therefore for the units:

N = [N^2/m^2]/[kg/m*s^2] = N^2*s^2/kg*m = N^2/N = N

So nothing is missing, there is no average chord there.
Actually I just tried the same check in English units and it all works out the 
same:

lb = [lb^2/ft^2]/[slug/ft*s^2] = lb^2*s^2/slug*ft = lb^2/lb = lb

You did not need to convert mass density into weight density.

I stand by my previous statement: that total induced drag does not depend on 
the 
AR for a fixed span (which is aero 101 really).
And I just learned something about English units!
Best regards,
Oleg.

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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Oleg Golovidov

A number of things trade off. As aspect ratio goes up,  Cavg goes down while 
W/L goes up (both numerator effects). Meanwhile, V^2 goes  up (denominator 
effect) as W/L goes up for a relatively constant Cl (assuming  the plane 
maintains approximately the same AoA at min sink or max L/D, whichever  you 
choose). 

Dave, Just noticed another strange assumption in your arguments.
I don't see how increasing AR changes W/L. It is constant unless you want to 
account for mass changes due to AR changes, which is true in reality, but again 
for a fixed span the weight of the wing is usually proportional to the wing 
area, therefore W/L will actually decrease for higher AR (smaller wing area).
Regards,
Oleg.

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Re: [RCSE] 2 meter and how it fits

2005-02-18 Thread Justin Ammon
What Mike said!!!
My new custom 2M is on the board.
I love my Open Class ships, but I really enjoy the challenge of 2M.  A high 
placing finish with a 2M means much more to me than the same finish with an 
open class ship.  I'll keep both spans and be very happy flying both (and 
RES too).

There is room for everybody.
Justin Ammon CEO
EdgeRC Inc
480-593-2458
www.edgerc.com
[EMAIL PROTECTED]
Practice does not make perfect...Only perfect practice makes perfect.
- Original Message - 
From: Mike Stump [EMAIL PROTECTED]
To: soaring@airage.com
Sent: Friday, February 18, 2005 5:49 AM
Subject: [RCSE] 2 meter and how it fits


After lurking and reading the many comments re 2 meter at the NATS I 
figured it was time to submit my dime's worth..

Let's first look at how 2 meter differs from the only other TD class 
(unlimited).. Because there really are just 2 true model classes for 
soaring for the major TD classes at the NATS (based on wing-span of 
course)... Again, these are based on wing-span, just like our full-scale 
counterparts...

With the span limited to 2-meters as compared to unlimited planes we're 
working with the following span-based performance limitations

less aspect ratio, limited visual profile at a distance, shorter glide 
ratio,  generally higher wing loadings.

This creates an entirely different flying environment and potential 
strategy for dealing with a given task. As I've read from a couple 
contributors, the limitation of size makes the 2 meter a bit more 
difficult to achieve a given task at times. This is something that makes 2 
meter unique as compared to unl. span planes, whether full-house or 
limited function (the RES class)...

One of the tenets laid out by Dan Pruss was that a soaring champion should 
show abilities in multiple disciplines and various aspects of Soaring.. 
Within the practical realm of the Soaring NATS in which we deal, 2 Meter 
is the other discipline.. There is no other.

If you take a look at our recent NATS Champs, the Dan Pruss Award has 
required excellence in both disciplines.. This should not change..

There have been other numerous comments referring to 2 meter as an entry 
level class. While it's true that many of us started with 2 meter planes 
like the Gentle Lady, in fact they were RES planes. At the NATS level, the 
competitive end of 2 meter can't be viewed as such.

The entry level category (and throw-back class) is RES. It was before it 
became a rule-book category.

Those that were involved in the early years of the present NATS structure 
might remember that we added RES/NOS at the end of the NATS week as sort 
of a laid back way to finish the week, replacing Sportsman's F3B (which 
occasionally was anything but). It was an easy day of relaxed competition 
before we all went home.

If we want more RES rounds, maybe we should fly just RES on the last day. 
There is a fair amount of cross-over/redundancy on RES/NOS day anyway. 
Maybe another event (like one of the Woody Majors) could host a 
Nostalgia Championship for those so inclined.

my dimes worth
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Re: [RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread John Erickson
Is the problem the term aspect ratio?  For his project he's probably using a
plank wing.  Aspect ratio is a term that can be applied.  What happens to
the same span if the planform becomes elliptical?  Do you still apply the
same aspect ratio?

Out of practical experience there is a big difference between a plank and an
ellipse, even with the same foil (most noticeable at higher speeds).

I think we've spun away from the original premise of how aspect ratio and
glide rate are related, but it's obvious that more variables quickly come
into effect.

I did a similar science fair project in high school where I tried two
different foils on the same planform and airframe.  I used the school gym,
turned out the lights and recorded the flight by leaving my camera lens open
and using a strobe light.  The project basically proved that the break
through airfoil I was trying didn't work at all.  The fact that I got to
integrate a glider and photography was probably more important.  I still
have one of my favorite pictures, where the glider was flown, banked hard
left towards the camera and flew by, all recorded by the strobe.  I think I
was blinking for about a week after that project.

JE
--
Erickson Architects
John R. Erickson, AIA


 
 I stand by my previous statement: that total induced drag does not depend on
 the 
 AR for a fixed span (which is aero 101 really).
 And I just learned something about English units!
 Best regards,
 Oleg.
 

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Re: [RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Thomas Koszuta
Sorry,
   The attachment seems to be prohibited by the newsgroup.  I will make the 
attempt soon or later to get this on my website, but for now, I will honor 
e-mail requests for those who need the documents.

   Or should I e-mail it to the exchange??? (one no and I will not)
Tom Koszuta
Western New York Sailplane and Electric Flyers
Buffalo, NY
- Original Message - 
From: Thomas Koszuta [EMAIL PROTECTED]
To: Soaring@airage.com
Sent: Friday, February 18, 2005 1:27 PM
Subject: Re: [RCSE] Re: Optimum aspect ratio - induced drag and span


There was a study done by Blaine K. Beron-Rawdon of Envision Design, at 
least a few years ago.  I will post this to news:rec.models.rc.soaring 
for your perusal.  The study spanned several wingpans and aspect ratios 
and has a document that summarizes the results.

E-mail if you need a copy directly.
Tom Koszuta
Western New York Sailplane and Electric Flyers
Buffalo, NY
- Original Message - 
From: [EMAIL PROTECTED]
To: [EMAIL PROTECTED]; Soaring@airage.com
Sent: Friday, February 18, 2005 12:59 PM
Subject: [RCSE] Re: Optimum aspect ratio - induced drag and span


So which term dominates is not completely clear without running  through 
a
bunch of numbers and making some estimates of weights, planforms, etc.
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[RCSE] Breakdown of Wood Crafters 05 enteries.......

2005-02-18 Thread Ray Hayes
Gentlemen,

Here is the breakdown of how the Wood Crafters 05 participants have chosen
to have fun flying their woody sailplanes at the AMA flying site in Muncie,
IN , May 26 thru 29, 2005.  Hopefully, this will give other persons or clubs
insight into the events people enjoy and incorporate these ideas into their
future events.

Without a doubt, Wood Crafters is all about having fun with woody
sailplanes and flying with woody enthusiasts.  This years event will have
some additions, changes and deletions from what we did last year.

Ch 11, 42, 45 are available for the Thursday and Friday Soar In Reunion and
the Saturday and Sunday Soar In Championship.  Contact me if you want to
play on one of these open freq.


Soar In Reunion event entries:  2 Minute Ladder  30,   Longest
Flight  26,   Fun Fly Only  1,  Man on Man 60  Mini Hi Start  16,   Man on
Man  Windfree Ray's Hi Start  7,Man on Man Ray's Mini Fun Scale (64)
Mini Hi Start  7,

Soar In Championship Class entries:Scale  21 (Gordon's Rules 8,
Ray's Fun Scale 13),
Best OLY ll   10,  Best Challenger   6, Best Astro Jeff   5,
2 Meter Unlimited   25,100 RES   34,Unlimited   35.

Special Awards:  People's Choice for Best Scale  and Wood Crafter's Award to
person selected for Outstanding Contributions to the promotion of RC
Soaring.

Free Drawing for Bench size Drill Press and other electric wood working
tools and various other prizes.

Nothing but fun at Wood Crafters 05

For More Wood Crafters info  .. go to the Wood Crafters page on my Sky Bench
web site.

Ray Hayes
http://www.skybench.com
Home of Wood Crafters

Ray Hayes
http://www.skybench.com
Home of Wood Crafters


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Re: [RCSE] ATTN: Sharon 3.7 x-tail owners, need input

2005-02-18 Thread Tom Hoopes


At 10:26 AM 2/18/05 -0600, Stan Myers wrote:
Had all but decided on Tempest when
the water got muddy. Someone(read Edgar Soaring Junkie)
suggested I consider the Sharon. So, I'm asking for input.
Probably the main criteria I have is that it be able to hi-start. I
do not have a winch readily available to me(and the club winch has seen
better days). I am able to get 23#'s of pull out of my hi start. Which
was adequate for my Artemis 5mph +, but really iffy for 1-3 
mph.
That aside, does it require constant attention with the sticks? I'm
a Sunday Flyer and I am looking for 'relaxed' flying. I
have some open class flying experience. I have a Sun 3.2m
electric powered by Hacker 50 that I am able to handle, but never really
got comfortable with the Artemis V tail.
Any and all suggestions would be appreciate.
Yes I'm the same guy who asked about the Tempest last week. Appreciate
the band width.
Stan

Stan,
I have a Sharon, Artemis and a couple of Icons so I might be able to
provide some input.
I bought my Sharon for an early morning/light lift F3J tool.
The Sharon will handle a brutal two-man tow without complaints. I'm not
sure what you would consider constant attention to the
sticks, but I think the Sharon is a nice flyer, with one exception.
During landing, the Sharon doesn't like a lot of radical flap modulation,
I'm guessing that this is due to the large flap chord. Otherwise, she's
got great legs, hangs well in light conditions and is great fun to
fly.
I've regularly hi-started my Sharon on 25' of 1/2 tubing with 50' of
mono, but I'm probably pulling around 40+ lbs at launch. My Sharon came
with a fixed position towhook and I replaced it with an adjustable
version as well as pushing the CG aft quite a bit.
Interestingly, my Artemis Lite (v-tail) is still my favorite TD plane to
fly. 


Tom Hoopes - ([EMAIL PROTECTED])
 -- Hoopes
Designs -
Taking the hassle out of wing wiring harnesses

http://www.hoopesdesigns.com



[RCSE] For Sale - Extreme

2005-02-18 Thread Chuck Robinett
Selling my back up Extreme cross tail sailplane.  This is the LT version in 
yellow and dark blue.

The wing and tail are practically new with very few flights. It is equipped 
with HS 125 superflat on the ailerons,  JR 368s on the flaps and elevator 
and a HS 81mg for the rudder. Includes Hitec Super Slim receiver and 1100ma 
battery. A set of individual wingbags available as an option.

Asking $1075 for RTF plus shipping.
E-mail me at [EMAIL PROTECTED] for questions.
Thanks
Chuck 

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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread RegDave
In a message dated 2/18/2005 12:47:33 PM Central Standard Time,  
[EMAIL PROTECTED] writes:
D(N) = [ W(N)/L(m) ]^2 /  [Pi*q(kg/m*s^2)],

(note, that W = m*g (N = kg*m/s^2)), therefore for the  units:

N = [N^2/m^2]/[kg/m*s^2] = N^2*s^2/kg*m = N^2/N = N

So  nothing is missing, there is no average chord there.
 
**

Oleg,

OK, we've got a nomenclature difference (it's always the communication  
issues, isn't it?)

My standard usage is W/L as Wing Loading which is  Weight / Area = Weight / 
(Span * Cavg)

I believe your W/L refers to the  Weight (W) divided by the Span (L) (- which 
I usually call S). Hopefully this  clarifies things. If you multiply the 
W/L term by Cavg/Cavg you get
 
Cavg * Weight / (L*Cavg) = Cavg * Weight / Area 
 
and things are consistent. Works the same in english, cgs, mks,  etc.

Sorry for the digression but with this sorted out, the result is  
mathematically the same. The reason I prefer to keep it in the wing loading  
form is 
that the scaling is a bit more apparent (to me). The lift force equation  
relates these two as:

Weight/Area (wing loading) = q * Cl 

(since  Lift has to equal Weight for steady flight)

Since q contains the V^2  term, Wing loading is proportional to V^2. - 
assuming Cl stays about the same.  The derived Drag formula then scales as

W^2 / L^2 / V^2  ~   Cavg^2 * Wing Loading)^2 / V^2

or 

Drag (induced) scales as Cavg^2  * (Wing Loading)

For a fixed span, as aspect ratio increases, the wing  loading does not go up 
as fast as Cavg goes down so Cavg wins. For a fixed Cavg,  as aspect ratio 
increases, wing loading will go up so drag should increase  (??)
 
 
*
I don't see how increasing AR changes W/L. It is constant unless you want  to 
account for mass changes due to AR changes, which is true in reality, but  
again 
for a fixed span the weight of the wing is usually proportional to the  wing 
area, therefore W/L will actually decrease for higher AR (smaller wing  area).

*
 
Again, this really depends on the assumptions one makes when doing an  
analysis. This was discussed most recently in RCSD, I believe the Jan 2004  or 
Feb 
2004 issues for a 2M design (server seems to be down right now but  available 
as PDF files form the general site: _http://www.b2streamlines.com/RCSD.html_ 
(http://www.b2streamlines.com/RCSD.html) .)
 
My assumption is that you have to look at the entire package. That means  
keeping a constant weight for the fuselage and radio equipment, and scaling the 
 
wing and tail surfaces for aspect ratio (constant volume coefficients are good 
 enough for the stabs). If you weigh all of those components, you'll usually 
find  that the wing is less than half of the total aircraft weight (take out 
the  servos and it's even less). So as you scale down the wing area, the weight 
of  the whole aircraft doesn't come down linearly with the wing area.
 
Since those analyses were for a fixed class (2M, for instance), as you  
change Aspect Ratio, you reduce the average chord at a fixed wingspan. Although 
 
the wing weight scales down with area, the weight of the fuselage and ancillary 
 
equipment stays relatively constant. Thus the wing loading will go up.
 
If you let the span be unconstrained then the options are much more  
flexible. But when you get to the open class design, the improved  efficiency 
from the 
higher achievable aspect ratios (at a reasonable wing  loading) set them 
quite a bit apart from 2M. Here it's the aspect ratio and  loading effects that 
dominate, not Re. So bigger flies better, but not strictly  due to Re effects.
 

 
Meanwhile, I hope the science fair project is going OK!
 
 
Thanks - and sorry for the confusion on the terminology.
 
- Dave R
 
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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Oleg Golovidov
Dave,

OK, we've got a nomenclature difference (it's always the communication  
issues, isn't it?)

In my original message I said the induced drag is proportional to SPAN LOADING, 
not wing loading, for a fixed span wing. That is really all I am trying to show 
you:

Di = (W/L)^2 / (Pi*q), where

W = weight, L = span, q = rho*V^2/2


Sorry for the digression but with this sorted out, the result is  
mathematically the same. The reason I prefer to keep it in the wing loading  
form is 
that the scaling is a bit more apparent (to me).

You can keep it in any form you want, the result is the same, total induced 
drag 
is not dependant on the AR for a fixed span. This is really a simple 
aerodynamic 
axiom that does need to be argued about. I guess I am not a high enough 
authority to take my word on it :-)

For a fixed span, as aspect ratio increases, the wing  loading does not go up 
as fast as Cavg goes down so Cavg wins. For a fixed Cavg,  as aspect ratio 
increases, wing loading will go up so drag should increase  (??)

By using chord and wing loading you are just clouding the issue. Yes, W/L = 
W*C/S, but you cannot change C (chord) without changing S (area) for a fixed 
span. It is still SPAN LOADING, Weight/Span. And yes, wing loading DOES go up 
as 
fast as the chord goes down. Change AR all you want, you are not changing SPAN 
LOADING. This is just elementary algebra actually, not even aerodynamics.

My assumption is that you have to look at the entire package.

I agree. I was only correcting you on one point. Total induced drag does not 
depend on the AR, only on the span, weight, speed. I hope you can work out the 
algebra and convince yourself in that.

Best regards,
Oleg.

PS. Apologies to the list for dragging this issue so far. I was not really 
contributing to the original topic here, just could not let the incorrect 
statement go :-0

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[RCSE] Re: Optimum aspect ratio - induced drag and span

2005-02-18 Thread Mark Holm
I didn't go through it to see if this looks like the source of 
confusion, but don't forget that bugaboo of English units, the 
pound-force.  Commonly abbreviated lbf, the pound force is defined as 
the force required to accelerate one pound-mass at a rate equal to l 
standard G, 32.17417 foot/second.

If you write pound, and are not careful to specify whether you mean one 
pound-mass or 32.17417 pound-mass foot / second^2, you can get mighty 
confused.

Most people don't even know there is a difference, of course most people 
don't know what accleration or force are and couldn't tell you the 
difference between their mass and their weight.

Though raised in the English unit U.S., I always go metric when I want 
to be sure of not screwing up a units calculation.  Gotta love the way 
so many of the conversion factors are exactly one.

Only idiots and engineers use poundals.  That is just asking for 
trouble, sometimes trouble in the multi-millions of dollars.

I have seen people use the kilogram-force as a supposedly metric unit. 
I think that is another stupid way to get into trouble.  Use Newtons. 
Once you figure out what they mean, and how to use them, you too will 
appreciate the beauty of a system that has most of its units convert by 
factors of one, and that does not stick some oddball number, like Earths 
gravity, into a basic unit.

Yes, I know the metric units are wholly arbitrary, but they are 
arbitrary in a whole lot less confusing way than English units.

--
Mark Holm
[EMAIL PROTECTED]
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Re: [RCSE] 2 meter and how it fits

2005-02-18 Thread Bob Johnson

After lurking and reading the many comments re 2 meter at the NATS I 
figured it was time to submit my dime's worth..

Let's first look at how 2 meter differs from the only other TD class 
(unlimited).. Because there really are just 2 true model classes for 
soaring for the major TD classes at the NATS (based on wing-span of 
course)... Again, these are based on wing-span, just like our full-scale 
counterparts...

With the span limited to 2-meters as compared to unlimited planes we're 
working with the following span-based performance limitations

less aspect ratio, limited visual profile at a distance, shorter glide 
ratio,  generally higher wing loadings.

This creates an entirely different flying environment and potential 
strategy for dealing with a given task. As I've read from a couple 
contributors, the limitation of size makes the 2 meter a bit more 
difficult to achieve a given task at times. This is something that makes 2 
meter unique as compared to unl. span planes, whether full-house or 
limited function (the RES class)...

One of the tenets laid out by Dan Pruss was that a soaring champion should 
show abilities in multiple disciplines and various aspects of Soaring.. 
Within the practical realm of the Soaring NATS in which we deal, 2 Meter 
is the other discipline.. There is no other.

If you take a look at our recent NATS Champs, the Dan Pruss Award has 
required excellence in both disciplines.. This should not change..

There have been other numerous comments referring to 2 meter as an entry 
level class. While it's true that many of us started with 2 meter planes 
like the Gentle Lady, in fact they were RES planes. At the NATS level, the 
competitive end of 2 meter can't be viewed as such.

The entry level category (and throw-back class) is RES. It was before it 
became a rule-book category.

Those that were involved in the early years of the present NATS structure 
might remember that we added RES/NOS at the end of the NATS week as sort 
of a laid back way to finish the week, replacing Sportsman's F3B (which 
occasionally was anything but). It was an easy day of relaxed competition 
before we all went home.

If we want more RES rounds, maybe we should fly just RES on the last day. 
There is a fair amount of cross-over/redundancy on RES/NOS day anyway. 
Maybe another event (like one of the Woody Majors) could host a 
Nostalgia Championship for those so inclined.
Hi Mike,
Thanks for your dimes worth. :)
I'm curious; who was it that suggested the criteria for the Dan Pruss Award 
should be different?

Regards,
Bob Johnson
Fond du Lac, WI 

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[RCSE] Test

2005-02-18 Thread Dan Kitching
Test. 

Seems awfully quiet this evening...
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