KR> Flap and belly board combination.

2011-08-04 Thread phil brookman
in my experience the kr flaps realy do something ===no doubt about it about 3 
knots ..
i am just looking at v g s ..possibly increasing wingspan a bit ==look at diehl 
wingskins 

phill






From: Peter Diffey 
To: KRnet 
Sent: Wed, August 3, 2011 10:16:56 PM
Subject: Re: KR> Flap and belly board combination.

Hi,

I am no expert, but as far as I can figure, a belly board will increase drag 
but 
will not increase lift, so will not allow a lower landing speed.

The belly board drag will allow a steaper approach, it will also help you bleed 
off speed during the roll out.

Whether the kr2 flaps have any significant effect on stall speed is a moot 
point, I doubt if anybody has done any design analysis.

Looking at the flaps on my std kr2 I doubt if they do much to stall speed.

The easiest way to keep down the safe landing speed is to build light - I 
thought hemlock was a sort of poison :)

Pete
-- 
Sent from my Android phone with K-9 Mail. Please excuse my brevity.

Rodger Nicolls  wrote:

Phil and Larry,
Thank you for the replies. I am looking at dropping the stall/landing speed,
increasing the visibility, and contending with a heavier empty weight (using
hemlock, 10% heavier than spruce, with extended fuselage). I have moved the
controls in front of the rear spar and plan to use the entire area behind
the spar for the flaps.
On anther note: I completed building my gear legs: 50 layers S-glass-BID and
38 layers S-glass-UNI, with a total compressed/cured thickness of .80". Now
I just need to get the mount welded.

If anyone is interested in the story (with pictures) of an experimental Cub
being destroyed by a calving glacier, let me know and I'll forward those to
you. It's a shame that after spending all that time on a lovely project to
see it lost in a matter of seconds.

I will continue to build.
Thanks,
Rodger
_

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KR> Flap and belly board combination.

2011-08-04 Thread Peter Diffey
I agree that they do help slow up.

They do alter the attitude which would indicate that there is something 
happening to the lift/drag ratio but I am not sure I would bet my privet hedge 
on the effect on stall speed :( I have wimped out of actually doing a full flap 
stall test.

In my experience landing distance is effected much more by weight. I can land 
happily in 400 yd on low tank, but with a full tank I just cannot get a good 
approach angle (even with full flap) and need up to 700 yds.

Of course this is a cg issue but any increase in weight needs more lift leading 
to increased angle of attach for a given speed which takes us close to the 
situation where the aot to take off is very close to the stall aot.

This all does my head in, so I would go with the old kiss mantra - light and 
simple.

Pete
-- 
Sent from my Android phone with K-9 Mail. Please excuse my brevity.

phil brookman  wrote:

in my experience the kr flaps realy do something ===no doubt about it about 3 
knots ..
i am just looking at v g s ..possibly increasing wingspan a bit ==look at diehl 
wingskins 

phill





_

From: Peter Diffey 
To: KRnet 
Sent: Wed, August 3, 2011 10:16:56 PM
Subject: Re: KR> Flap and belly board combination.

Hi,

I am no expert, but as far as I can figure, a belly board will increase drag 
but 
will not increase lift, so will not allow a lower landing speed.

The belly board drag will allow a steaper approach, it will also help you bleed 
off speed during the roll out.

Whether the kr2 flaps have any significant effect on stall speed is a moot 
point, I doubt if anybody has done any design analysis.

Looking at the flaps on my std kr2 I doubt if they do much to stall speed.

The easiest way to keep down the safe landing speed is to build light - I 
thought hemlock was a sort of poison :)

Pete
-- 
Sent from my Android phone with K-9 Mail. Please excuse my brevity.

Rodger Nicolls  wrote:

Phil and Larry,
Thank you for the replies. I am looking at dropping the stall/landing speed,
increasing the visibility, and contending with a heavier empty weight (using
hemlock, 10% heavier than spruce, with extended fuselage). I have moved the
controls in front of the rear spar and plan to use the entire area behind
the spar for the flaps.
On anther note: I completed building my gear legs: 50 layers S-glass-BID and
38 layers S-glass-UNI, with a total compressed/cured thickness of .80". Now
I just need to get the mount welded.

If anyone is interested in the story (with pictures) of an experimental Cub
being destroyed by a calving glacier, let me know and I'll forward those to
you. It's a shame that after spending all that time on a lovely project to
see it lost in a matter of seconds.

I will continue to build.
Thanks,
Rodger
_


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to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see other KRnet info at http://www.krnet.org/info.html

_

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KR> Flap and belly board combination.

2011-08-04 Thread Patrick and Robin Russo
Roger
  Our eastern Hemlock is close to the specific gravity (weight) of Sitka 
Spruce. The western hemlocks are about 8-10 percent heavier. We use the 
hemlock here in Vermont for barn construction. The disadvantages of hemlock 
might be 1- the lower elastic strenght, about 25% lower which means the wood 
will split instead of flex.  2- It doesn't laminate (take to glue)as readily 
as Spruce and 3-the diffuculty in finding nice straight grained stock which 
can lead to twisting, distorting etc. before the pieces are locked in. As an 
example, cut 2 pieces of Hemlock 5/8"thick x 2" wide x 4'Long. Let them sit 
about the shop for 2 weeks and you will find that they are no longer equally 
straight. That is not good if they are stabilizer or wing spars. Having said 
this, hemlock will work, it will not dry rot as readily as spruce.
   I did make a gear spring as you describe, 55 layers in all of Bid and 
uni, came out to 7/8" thick and weighed in 20% heavier than the cessna 
spring I was copying and was not as stiff. I was surprised. Perhaps I used 
too much resin. I also put it on a press to see how easily I could break it. 
It did split along the layers...but not fatally
Pat R
- Original Message - 
From: "Rodger Nicolls" 
To: 
Sent: Wednesday, August 03, 2011 1:05 PM
Subject: Re: KR> Flap and belly board combination.


> Phil and Larry,
> Thank you for the replies. I am looking at dropping the stall/landing 
> speed,
> increasing the visibility, and contending with a heavier empty weight 
> (using
> hemlock, 10% heavier than spruce, with extended fuselage). I have moved 
> the
> controls in front of the rear spar and plan to use the entire area behind
> the spar for the flaps.
> On anther note: I completed building my gear legs: 50 layers S-glass-BID 
> and
> 38 layers S-glass-UNI, with a total compressed/cured thickness of .80". 
> Now
> I just need to get the mount welded.
>
> 


KR> Flap and belly board combination.

2011-08-04 Thread cgardn628
KR Heads,

Regarding the "postage stamp" size flaps on the KR2S, I built them in and I
would disagree. They are useful in lowering the stall speed by maybe 5 mph
in stall tests I have done at altitude. Glad I made the effort to build
them.

They also are a big help to forward visibility when landing ( nose down
view). I wish I had also installed the belly board to reduce the floating
down the runway syndrome in ground effect.

Cheers

Chris G KR2S 250 hours 

-Original Message-
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of Peter Diffey
Sent: Wednesday, August 03, 2011 5:17 PM
To: KRnet
Subject: Re: KR> Flap and belly board combination.

Hi,

I am no expert, but as far as I can figure, a belly board will increase drag
but will not increase lift, so will not allow a lower landing speed.

The belly board drag will allow a steaper approach, it will also help you
bleed off speed during the roll out.

Whether the kr2 flaps have any significant effect on stall speed is a moot
point, I doubt if anybody has done any design analysis.

Looking at the flaps on my std kr2 I doubt if they do much to stall speed.

The easiest way to keep down the safe landing speed is to build light - I
thought hemlock was a sort of poison :)

Pete
-- 
Sent from my Android phone with K-9 Mail. Please excuse my brevity.

Rodger Nicolls  wrote:

Phil and Larry,
Thank you for the replies. I am looking at dropping the stall/landing speed,
increasing the visibility, and contending with a heavier empty weight (using
hemlock, 10% heavier than spruce, with extended fuselage). I have moved the
controls in front of the rear spar and plan to use the entire area behind
the spar for the flaps.
On anther note: I completed building my gear legs: 50 layers S-glass-BID and
38 layers S-glass-UNI, with a total compressed/cured thickness of .80". Now
I just need to get the mount welded.

If anyone is interested in the story (with pictures) of an experimental Cub
being destroyed by a calving glacier, let me know and I'll forward those to
you. It's a shame that after spending all that time on a lovely project to
see it lost in a matter of seconds.

I will continue to build.
Thanks,
Rodger
_

Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see other KRnet info at http://www.krnet.org/info.html

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KR> Static Test Results

2011-08-04 Thread Dave Dunwoodie
OK, I've been silent, busily working away, and today I managed to get 
some repeatable numbers.  I would appreciate "health" checks from 
any/all of you!!!

Engine:  Revmaster 2100D
OAT:  81 F.
Humidity: 63%
Elevation: 920'

Engine Run Duration: 20 Minutes
Cowl Flap Open
Ram air closed
RPM 1700

Peak Temperatures Noted:
OIL: 210
CHT: 400
EGT: 1025
(These figures were obtained with the mixture leaned.)

Mixture full rich:
OIL: 200
CHT: 350
EGT: 950

Thanks for any thoughts!

Best Regards,

Dave.



KR> Fuel System

2011-08-04 Thread Dave Dunwoodie
I am still undecided about the fuel pump after struggling with it for a 
year.  It is the Facet that has been recommended by several people.

When first installed, I noted that it would nearly flood the engine and 
that an immediate leaning of the mixture was required whenever it was 
turned on.  I solved this one by installing a 5/32" bypass line from the 
pump outlet back to the header tank.  Mixture adjustments from pump on 
to pump off are now minimal.

With the pump off, I can cause the engine to stall at higher RPM by 
setting full rich and waiting.  It seems the free-flow (gravity only) 
rate through the pump is just barely adequate and eventually the 
gascolator empties and the engine stalls.  I can always remedy this by 
turning the pump on for a couple of seconds, so I am convinced it is a 
fuel starvation situation.

I installed a "T" before and after the pump, and made another bypass, 
5/16" diameter with a one-way valve.  With the pump off, the theory is 
that fuel will flow from the header tank through the one-way valve and 
out to the engine.  This effectively creates two flow paths from the 
tank to the engine.  Even with this, I heard the engine stutter a little 
after about 15 minutes with no pump.  Again, just bumping the pump for a 
couple of seconds cleared the situation.

I am very close to reverting to gravity only feed, and am interested in 
who runs gravity only, and what, if any, obstacles they had to 
overcome.  My main concern has been vapor lock, and the pump is very 
effective at clearing situations like this.  However, getting adequate 
fuel flow when the pump isn't running has developed into a real 
challenge.  If I keep the pump, my preference is that it NOT be used for 
normal operations.

What have you that use gravity only encountered in your low fuel 
situations, climbs, etc.?

The entire fuel system has been cleaned and cleaned again, new filters, 
everything.  So it appears that I'm fighting purely a flow situation 
when the pump isn't running, and not some unknown restriction or blockage.

Any thoughts or comments would be appreciated.

Thanks,

Dave.




KR> Fuel System

2011-08-04 Thread phillipmathe...@bigpond.com
When first installed, I noted that it would nearly flood the engine and
that an immediate leaning of the mixture was required whenever it was
turned on.  I solved this one by installing a 5/32" bypass line from the
pump outlet back to the header tank.  Mixture adjustments from pump on
to pump off are now minimal.
-

Facet come in all different PSI pressures.

My carb  ONLY needs 3psi. So find out what you need and buy a inline 
pressure reduction, or but the correct pressure pump.

I have a great unit one on my KR but I am away at the moment and can not 
remember the name.

Phil Matheson
Australia. 



KR> wing tip slop

2011-08-04 Thread phillipmathe...@bigpond.com
Martin

I'm in melb for a few days. How are you. Any more news on the Damage, Can it 
be fixed.

Phil Matheson 



KR> hello kr

2011-08-04 Thread Virgil N. Salisbury
On 8/2/2011 11:33 PM, joseph lamberson wrote:
> hey kr check it out http://nbcllnews.com/?article=924381
>
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>
Not another one, Virg


KR> Diehl Gear for sale.

2011-08-04 Thread joemals...@charter.net
bob,

I am interested, Contact me on my email.
joemals...@charter.net

joe.

On Tue, Aug 2, 2011 at 11:25 PM, badbob0...@embarqmail.com wrote:

> I have the tricycle Diehl landing gear AND  Tracy O?Brian C-90 brakes, 
> Cessna style axles, TriStar 5? wheels (3) and Shen tires. These are 
> all in new condition. The current retail for these is in excess of 
> $2000.00. I would entertain offers in the $1600.00 range OBO.
>
> Bob Johnson
> Willamina, OR
> (971) 645-9491
>  https://picasaweb.google.com/103552664644911775549/KR2SSW 
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KR> Flap and belly board combination.

2011-08-04 Thread Mark Langford
Pete Diffey wrote:

>Looking at the flaps on my std kr2 I doubt if they do much to stall speed. 
>Whether the kr2 flaps have any significant effect on stall speed is a moot 
>point, I doubt if anybody has done any design analysis.<

You mean you have flaps installed on your plane and have never done a stall 
speed test with them retracted and also with them deployed?  You have the 
perfect test device at your disposal, yet haven't actually tested it? 
Then you have very little useful data to contribute on the issue, I'd say. 
Analysis and conjecture is one thing, but real-world testing tells the 
story...

Mark Langford
ML at N56ML.com
website at http://www.N56ML.com