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Automotive |
11-98
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| Technical
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Students pull off a cunning stunt
Lou Reade
watches the latest progress of an aeroplane whose design stretches back
30 years
Think back
to or even consult the final year project you carried out
as a student. For the older ones among you, the hand-drawn designs will
be peppered with quaint references to foot-poundals and dynes. But no
matter how inspired or professional, very few will have the makings of
a full commercial product.
But one project
from 30 years ago has moved with the times. Cranfield University is celebrating
the completion of the A1-200, a specialist aerobatic plane that grew out
of a specification put forward in 1968 by Neil Williams, then the UKs
top stunt pilot. Williams specified a plane that would compete with the
cream of stunt planes of the time most of them from Russia. For
several years, the design codenamed the A1 was little more
than an ongoing research project for students.
Professor
Denis Howe, who oversaw the project back then and is still at the department,
says: "Students in successive years have worked on the project. Its
been handed on from year to year, almost like a baton."
In these
early days, Prof Howe admits that his main job was to manage the process
and persuade supporters to come on board. For a long time, the project
remained within the department as he struggled to attract outside interest.
Seven years on, an aerobatics enthusiast, Alan Curtis, stepped forward
with £20,000, allowing the drawings of the plane to make it into production
at last.
The first
version of the plane was a single seater with a 210 horse power engine.
It was registered in 1978. A constant feature specified by Williams
which holds to this day was a wing span of exactly 10m.
The second
version boasted a larger engine, 270 hp, and improved controls, which
would allow better manouevring though Williams said the plane still
needed to improve its flick roll performance. Meanwhile the
A1 MkII did the rounds of aerobatic shows.
But Williams
was killed in 1977, after which the project languished. But the flick
roll problem was eventually solved and in 1994, Cranfield began a part-time
MSc course for British Aerospace employees. The three year course included
individual research projects and group design projects for which
an extension of the A1 project was ideal.
This time,
the design would incorporates a passenger seat, increase engine size and
add a second fuel tank.
"The
job was to modify the A1 MkII into a two-seat configuration," says
Robert Jones, lecturer in air vehicle technology and project leader for
the A1-200 at the college.
The group
split into three competitive teams, which each looked at how the existing
design needed to be modified in order to meet the new specifications.
All the teams concluded that tweaking would be no good
large scale modification was necessary.
This led
to a set of affordable modifications being proposed, which
the teams could then work on. These included changes to the canopy, trailing
edge flaps and electrical system. At the same time, another team looked
further, at major modifications which would help the
teams to get closer to the full requirements of the plane. These included
a composite wing design and a composite fuselage.
Now that
the A1-200 is finished and the students have graduated, a fourth version
of the plane is in the pipeline to be worked on by the latest intake
of MSc students. The A1-400 needs a better lateral response,
which means fitting a new fin and rudder making them from composite
materials rather than the existing aluminium alloy. The A1-400 project
is much shorter Prof Howe believes that it will be ready early
next year.
He points
to the "enthusiasm and drive" of the students that work on this
project and when you stand watching the fruit of their labours
doing back flips and other aerobatic manoeuvres above you, you can understand
why.
Differences
between the A1 MkII and A1-200
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A1 Mk II
|
A1-200
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| Max level speed (m/s) |
76
|
80
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| Climb rate (m/s) |
13.5
|
12.5
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| G limits |
+7/-5
|
+6/-3
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| Roll rate (deg/s) |
150
|
160
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| Range (km) |
238
|
800
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| Stall speed (m/s) |
25
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25
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