Bill,
I came a little faster on my second
landing (second flight) and greased it on.
I am using the fix published by the Mustang II designer, Bob Bushby, in
an early newsletter, which is to make the leading edge of the outer 1/3 of the
wing that drops - more round, i.e. not as sharp. This allows the air to flow over the
leading edge more easily at higher angles of attack without separating from the
wing and lets the wing keep flying longer.
After my initial re-work effort, the right wing drop at stall was much
less severe on the second flight and the plane more stable leading up to the
stall. The right wing still drops
first, so I plan to continue rounding the outer leading edge of my right wing
per Bob Bushby’s method until both wings stall at the same time.
The radiator and oil cooler are located between
the engine and the firewall, much like the Powersport installation http://powersportaviation.com/rv-6a_n225ps.htm
Here is a link to my engine installation before
the baffling was installed that forced all air to pass through the radiator and
oil cooler before exiting the engine compartment. http://www.eaa1246.org/big_photo.asp?id=Turbo%2Ejpg
Bob
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bill Bradburry
Sent: Monday, March 30, 2009 7:12
PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: Video of
First Flight - Mustang II w/ 13B Rotary Engine
Bob,
You are correct about that wing drop. I ran your video several
times to see if the wing tip had hit. It was good that you were only a couple
of feet off the ground when it did that roll. Be sure and keep the speed
up till you are ready to touch down. Do wheel landings with that tail
dragger. Plant it on the ground still flying. You say you have
modified the wing some already??
4800 rpm with that 84 pitch should work out to about 176 mph with no
slippage, so you are right in the ballpark. That means that you would get
close to 220 mph at 6K rpm! That is going to be a really fast plane!
Where are your radiator and oil cooler located? Do you have any
pictures of that install?
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Rogers, Bob J.
Sent: Monday, March 30, 2009 12:08
PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: Video of
First Flight - Mustang II w/ 13B Rotary Engine
Ed,
On takeoff, the turbo engine was producing
38 inches of manifold pressure and I still had 1/3 of my throttle left.
Because I have an aggressively pitched prop (68x 84), I think there was a
little blade stall until I got more speed. I climbed out at 120 mph and
over 1,000 fpm. I did not feel any “P” effect, but I may have
been too excited to notice. The controls are well balanced and the plane
will stay wherever you point it, hands off. My only problem so far is
that the right wing stalls first and causes a sharp wing drop. The
published fix is to make the outer leading edge more rounded on the right
wing. After some re-shaping, the stall was much improved on the second
flight, but I still need to do a little more work on the right wing to get it
to stall at the same time as the left wing.
The nose is longer than usual. I moved the
seats back some and added additional baggage space behind the seats, which called
for more weight on the nose. Based on my original W&B estimates, that
is where the engine should have been placed. It gave me enough room to
place the radiator and oil cooler between the engine and firewall.
As it turned out, the plane was slightly nose heavy with the battery on the
firewall, so I repositioned the battery in the tail. Now the W&B is perfect.
As a bonus, the battery is out of the engine compartment where it would have
gotten a lot of heat and there is more room on the firewall for cooling air to
exit. So far, I have been able to idle on the ground for over 25 minutes
without any overheating. My cowl flap can be opened wide or closed to
adjust for temperature needs. Even on climb out, the engine barely got up
to operating temp (180 degrees) with the cowl flap half open. Yesterday,
on the second flight, I closed the cowl flap completely and ran the engine up
to about 32 inches of manifold pressure and got 190 on water temp after about
five minutes. Speed was only 170 mph (4800 rpm) at 3,500 feet and OAT was
55 degrees F. When it gets hot during the summer months, cooling may be
marginal at high power settings. With the turbo, I should be able to fly
at higher altitudes where it is cooler and I can go faster. Time will
tell. Right now, I am happy just to be flying instead of building.
Bob
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Monday, March 30, 2009 9:32
AM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: Video of
First Flight - Mustang II w/ 13B Rotary Engine
Great looking flight, Bob!!
Looks like you took off less than WOT
during initial roll and then applied more power near/after lift off based on
the sound track I heard. I presume appreciable “P” effect?
Let us know what the numbers look like on your next flights – temps as
well as performance.
Great to see a project get airborne,
congratulations again!!
Best Regards
Ed
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Rogers, Bob J.
Sent: Monday, March 30, 2009 10:13
AM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Video of
First Flight - Mustang II w/ 13B Rotary Engine
If you are interested, there is a video of my first flight
at this link. http://www.eaa1246.org/videodisplay.asp?id=36
I have a lot of good friends who helped me make the event a
success. They took pictures and video and were there to support me.
I did my second flight yesterday and all went well.
The landing was much better.
Bob
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