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New topic - spin off of prop discussions

 
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drc(at)wscare.com
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PostPosted: Fri Jul 20, 2012 10:48 am    Post subject: New topic - spin off of prop discussions Reply with quote

I would be interested to hear from pilots that have experience with both the 50 and the 55.
How would you compare aerobatic capabilities -
Verticle / roll / induced drag / balance of CG to center of lift ??

Even maintenance and value??

If anyone can compare to SU 26 it wold be an interesting comparison. I read an old article that was a great review of the SU26 / Yak 55, but would be interested to hear from someone who also could compare Yak 50.

Thanks,
Herb


Dr. Herb Coussons, MD
drc(at)wscare.com
2641 Development Drive
Green Bay, WI 54311
Cell 920-639-8434
Work 920-338-6868
Fax 920-338-6869


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richard.goode(at)russiana
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PostPosted: Fri Jul 20, 2012 8:03 pm    Post subject: New topic - spin off of prop discussions Reply with quote

The 50 and 55 are very different aircraft. In my view, the 50 is one of the
world's classic aircraft, but it was unfortunate that it came out in 1976,
just as aerobatics was changing from being big, gracious manoeuvres to
vicious corners. It is a tough aircraft, +9 and -7, but the Russians were
flying well beyond those limits and suffered a number of airframe failures.

The 50 is a delight to fly, and has that feeling of a little "fighter". But
the controls are poorly harmonised, with a very light elevator and heavy
ailerons. The latter can be helped with the wingtip "spades", but they're
not terribly attractive.

It was a combination of structural problems and high rates of roll from
Western competitors that brought about the 55, which is very different. It
is immensely strong, and for its money, the best aerobatic plane you can
buy. But even its best friends would not say that it is beautiful!.

When the 55 came out all 50s were ordered to be cut up - hence we are left
with about 65 of the total production of 307.

My personal view is that the long wing 55 is a nicer, and in many ways more
effective aircraft than the clipped - wing 55N, which was a rather desperate
measure to try to keep up with the Sukhoi 26. The problem about the shorter
wing is that it has much higher induced drag. So, although the long wing is
slower in roll, it will normally retain more height in the same sequence
than the "M".

I believe it is a mistake to see the 50 in the same context as 55 and Sukhoi
26. It is an older design, and an aeroplane for more gentle aerobatics and
"fun" flying. I'm sure that in the long-term, the 50 will become a very
valuable aircraft. On the other hand, the 55 and the 26 are much more
capable aerobatic aircraft - that is simply the advance of technology.

One does need to be careful about the modification status of 50s. I see
people writing about them having "the heavy spar" whereas there were a whole
series of modifications to attempt to keep up with the Russian Team
over-flying the aircraft. I have prepared a paper on these modifications,
and the problems that caused them if anyone is interested.

Remember, also, that the original G limits were for an aircraft with only
the small fuel tank; maximum weight of pilot and parachute 90kgs - 200
pounds, and without generator etc and without generator.I would not fly one
today beyond +6 and -4, and that for one with all mods embodied. Like that,
it will last for ever

Of course with retractable gear the 50 will be a bit more expensive to
maintain, but not by a huge amount.

Richard Goode
Rhodds Farm
Lyonshall
Hereford
HR5 3LW
United Kingdom
Tel: +94 (0) 81 241 5137 (Sri Lanka)
Tel: +44 (0) 1544 340120
Fax: +44 (0) 1544 340129
www.russianaeros.com
I'm currently in Sri Lanka but this Mail is working,and my local phone is
+94 779 132 160.
--


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jan.mevis(at)informavia.b
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PostPosted: Fri Jul 20, 2012 8:52 pm    Post subject: New topic - spin off of prop discussions Reply with quote

I'd liked to read that paper on the modifications for the 50, Richard!
Thanks,

Jan

On 21/07/12 06:01, "Richard Goode" <richard.goode(at)russianaeros.com> wrote:

[quote]
<richard.goode(at)russianaeros.com>

The 50 and 55 are very different aircraft. In my view, the 50 is one of
the
world's classic aircraft, but it was unfortunate that it came out in 1976,
just as aerobatics was changing from being big, gracious manoeuvres to
vicious corners. It is a tough aircraft, +9 and -7, but the Russians were
flying well beyond those limits and suffered a number of airframe
failures.

The 50 is a delight to fly, and has that feeling of a little "fighter".
But
the controls are poorly harmonised, with a very light elevator and heavy
ailerons. The latter can be helped with the wingtip "spades", but they're
not terribly attractive.

It was a combination of structural problems and high rates of roll from
Western competitors that brought about the 55, which is very different. It
is immensely strong, and for its money, the best aerobatic plane you can
buy. But even its best friends would not say that it is beautiful!.

When the 55 came out all 50s were ordered to be cut up - hence we are left
with about 65 of the total production of 307.

My personal view is that the long wing 55 is a nicer, and in many ways
more
effective aircraft than the clipped - wing 55N, which was a rather
desperate
measure to try to keep up with the Sukhoi 26. The problem about the
shorter
wing is that it has much higher induced drag. So, although the long wing
is
slower in roll, it will normally retain more height in the same sequence
than the "M".

I believe it is a mistake to see the 50 in the same context as 55 and
Sukhoi
26. It is an older design, and an aeroplane for more gentle aerobatics and
"fun" flying. I'm sure that in the long-term, the 50 will become a very
valuable aircraft. On the other hand, the 55 and the 26 are much more
capable aerobatic aircraft - that is simply the advance of technology.

One does need to be careful about the modification status of 50s. I see
people writing about them having "the heavy spar" whereas there were a
whole
series of modifications to attempt to keep up with the Russian Team
over-flying the aircraft. I have prepared a paper on these modifications,
and the problems that caused them if anyone is interested.

Remember, also, that the original G limits were for an aircraft with only
the small fuel tank; maximum weight of pilot and parachute 90kgs - 200
pounds, and without generator etc and without generator.I would not fly
one
today beyond +6 and -4, and that for one with all mods embodied. Like
that,
it will last for ever

Of course with retractable gear the 50 will be a bit more expensive to
maintain, but not by a huge amount.

Richard Goode
Rhodds Farm
Lyonshall
Hereford
HR5 3LW
United Kingdom
Tel: +94 (0) 81 241 5137 (Sri Lanka)
Tel: +44 (0) 1544 340120
Fax: +44 (0) 1544 340129
www.russianaeros.com
I'm currently in Sri Lanka but this Mail is working,and my local phone is
+94 779 132 160.
--


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