Mark
Thanks for the advice. I have studied your webpages for some time now
and it is clear you have good experience!
Regards
Deon
On 13/01/2017 02:18, Mark Langford via KRnet wrote:
Virg wrote:
> Pitch sensitivity is an overblown item, Virg
Now that I have put over 1100 hours on a KR2S, a
What Chris describes is not at all unusual. A number of aircraft fly better in
an aft CG as the elevator gets too heavy with a forward CG. A C-182 is a good
example. A 200 horse Muskateer is another. It flies better and is easier to
land if your CG is a bit aft simply because the elevator ge
> Could you go into further detail about "how" it flew better with a forward
> CG than an aft CG?
Sure, the plane under normal conditions (no baggage) would require
significant up trim to unload the stick, and when pulling power, would
drop the nose unless you held onto the stick. "Lawn dart"is a
Kayak Chris wrote:
> with all this talk about pitch sensitivity, one common mention is
> using forward CG. What is up with that? My last plane really liked aft
> CG (within the envelope obviously) and flew MUCH better there. What
> happens to a KR at aft CG?
You had an odd bird if it flew better
with all this talk about pitch sensitivity, one common mention is
using forward CG. What is up with that? My last plane really liked aft
CG (within the envelope obviously) and flew MUCH better there. What
happens to a KR at aft CG?
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At 03:45 PM 1/12/2017, you wrote:
Pitch sensitivity is an overblown item, Virg
++
Pitch sensitivity is NOT overblown but it also SHOULD NOT be an issue
for the knowing pilot. It is easily accommodated on the first flight
and actually m
Virg wrote:
> Pitch sensitivity is an overblown item, Virg
Now that I have put over 1100 hours on a KR2S, and almost 300 on a KR2,
I feel qualified to say that there is a pretty large difference in pitch
stability between the two. Yes, the KR2 is entirely controllable, but
then mine is flown
Pitch sensitivity is an overblown item, Virg
On 1/12/2017 10:42 AM, Deon-tsrc via KRnet wrote:
Hi Virgil
The KR2 apparently suffers from too much pitch sensitivity.
Later designs resulted in the KR2S which has a longer fuselage length
increasing the moment arm of the tail. An
Rick,
Here is the web page about building his pitot tube. Should give you
everything you need.
http://www.n56ml.com/fairings.html
--
Wayne DeLisle Sr.
KR> KRnet Digest, Vol 5, Issue 3
Rick Cochenet wiharley69 at yahoo.com
Sat Jan 7 11:52:24 EST 2017
Previous message (by thread): KR> FOR SAL
Hi Virgil
The KR2 apparently suffers from too much pitch sensitivity.
Later designs resulted in the KR2S which has a longer fuselage length
increasing the moment arm of the tail. Another idea was too increase the
surface area of the horizontal stabilizer (see Mark Langford's
discussion about
What pitch sensitivity ? Virg
On 1/12/2017 1:47 AM, Deon-tsrc via KRnet wrote:
Good day
I was thinking that in the process I should reduce pitch sensitivity by
enlarging the tail area as well. So removing the aft spar of the
horizontal stabilizer and install a longer one.
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