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Translated
from Italian
Engineer Luigi Stipa can certainly be included in the select number of
maverick
Aircraft Designers that Italy has produced, as he foresaw, as early
as 1931,
the possibility of jet propulsion that he tried to interrupt in an emanatory
way.
Luigi Stipa was born in Appignano del Tronto on the 30th November 1900
and
from his family farming background he learnt the philosophy of hard work
that
he was to apply throughout his life. Following his natural inclination
for practical
application he enrolled as an Aircraft engine fitter during WW1.
At the end of
the war he returned to his studies and graduated in Civil, Hydraulic and
Aeronautic
Engineering in 1924 and 1927. In 1928 he enrolled as NCO in the
Regia Aeronautic
to reach, eventually, the position of the Air Force Engineering Division
General
Inspector.
His background in hydraulic engineering convinced him of the possibility
of
successfully using hydrodynamic principles for aeronautical applications
and,
after 5 years of development, Stipa submitted to the Technical Division
of the
Air Ministry a design for a twin engine land/sea plane fighter.
The Regia
Aeronautica examined the proposal and funded the construction of a single
engine two seater ducted fan prototype.
Caproni
built the Aircraft, as per the Regia Aeronautica requirements, at their
plant near Milan in 1932. The unusual design caused a number of
sceptical
comments and the original design intention of increasing the efficiency
of the
propeller by reducing the losses was generally misunderstood.
The wide fuselage was
practically a tunnel with
a profile similar to the wings.
And could have been
considered to be a "circular wing".
A 120 HP Gipsy III engine was
mounted inside (left) a tapered duct
driving a two-blade tractor
propeller, in effect utilising the Bernoulli Principle related to fluids
moving in a venture
duct. Stipa idea was, in fact, a step towards the achient of jet
propulsion.
Princetown University Press published "High Speed Aerodynamics and
Jet Propulsion"
in 1959 and in Vol. XII stated "The Stipa Aero plane built
by Caproni in 1932 should
be classified as a Jet Aircraft. 'The Stipe Aero plane can be considered
as a
predecessor of the Jet Aircraft of today".
The
Test Pilot, Domenico Antonini, took off for the Test Flight at Caproni
Taliedo
on October 7 1932. His report was quite favorable, stating that
"the take off was
achieved easily after a 180 m run."
The
plane climbed easily and without vibrations, in level flight the Aircraft
exhibited
an exceptional stability. Antonini reported, "It
is difficult to make the Aircraft
move from the flight path." Landing was normal using approximately
the length of
runway used for take off. The Regia Aieronautica took over the Test
Program;
with the Aircraft having been transferred to the Test Flying Squadron
based at
Rome- Vionteceiio. The Regia Aeronautica Test Pilot, Olivari, confirmed
the original
Test Flight data and recorded his surprise at the minimal take off and
landing runway
required by the Aeroplane. He also underlined the unusual ratio
of 1.96 existing
between the minimum and max speed, at the time comparable only to the
Fiat A.S.1.
The
Regia Aeronautica however, decided that the advantages of the duct fan
were
not sufficientto continue with the development and the project was dropped.
Stipa was called to France in 1938 to develop his "Stipa 203"
fighter, but the start
of WW II ended this project. He patented the principle of the pulsating
jet engine
in 1938 in Italy, Germany and the United States and remained convinced
to his death
in 1992 that the Germans used his patent to develop the V-1 engine.
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