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By Christoph Hiemcke, Werner Seibert, S. Shashidhar, and Rajib Chakraborty,
Fluent Inc.
View the pdf of this article

Photo and sketches courtesy of National Air & Space Museum, Smithsonian
Institution (SI 2002-16646, SI 2000-4488)
December 17, 1903
Kitty Hawk, North Carolina:
With Orville Wright at the controls, and Wilbur supporting the right
wingtip, the 1903 Wright Flyer lifted off its launch rail to become the
world’s first powered, controlled, and manned aircraft.
Following years of patient and carefully conceived trials, the Wright
Brothers succeeded in pulling together all of the features required for
a successful airplane. They tested different kite configurations, invented
a wingwarping mechanism to permit banking of their air vehicles, systematically
evaluated airfoils mounted in front of the handlebars of a bicycle (they
owned a bicycle factory) and later in their own wind tunnel, flight-tested
manned gliders, built their own motor, and designed their own propellers.
Their achievement was not widely recognized for some time, mainly because
of the secrecy that surrounded it. In the meantime, other manufacturers
surpassed their design, especially through Glenn Curtiss’ introduction
of the aileron (a hinged flap for lateral roll control) instead of the
Wrights’ wing warping mechanism, and through an aft placement of
the elevator (an auxiliary airfoil used for pitch control) instead of
the Wright Brothers’ upwind placement. Interestingly, the Wrights
had initially placed the elevator in front of the pilot to improve the
responsiveness of their gliders; later, they kept it in this“canard
configuration” to protect the pilot during crashes, and to allow
him to observe the elevator during flight. The big problem with the canard
was that it made the airplane unstable, making it difficult for the pilot
to control the nose-up and nose-down motions.
In addition to their initial historic flight and the first use of canards,
the Wright Brothers can be credited with many firsts in aerospace engineering,
including the systematic wind tunnel testing of airfoils, the development
of a control system for banking airplanes, and the development of an effective
theory for airplane propellers.

Contours of pressure on the mid-plane of the Flyer
Postprocessing by Advantage CFD (www.advantage-cfd.co.uk)
using EnSight by CEI
December 17, 2003
Kitty Hawk, North Carolina:
One hundred years later, a repeat of the historic first flight is planned
using a replica of the Wright Flyer.
Aviation has come a long way in the past one hundred years, and the advances
in flight have only heightened the appreciation for the remarkable achievements
of the Wright Brothers. To commemorate these achievements, the centennial
year has featured a broad range of events and celebrations. Preparations
for these festivities began years ago, especially through efforts to construct
replicas of the 1903 Wright Flyer. Both wind tunnels and CFD were used
during the design of these replicas to improve engineers’ understanding
of the performance of the airplane components. One application of CFD
to the design of a Wright Flyer replica is the analysis of the performance
of the 1903 propellers with FLUENT (see the following story.) An important
goal was to fully anticipate the propeller aerodynamics at off-design
conditions.
To celebrate the centennial, Fluent engineers created a mesh of the
full aircraft, and computed the flow at the historic cruise speed of 30
mph. The model included most of the detailed features of the full Flyer,
such as all struts, the motor, and Orville at the controls, but did not
account for the deformation and permeability of the muslin fabric covering
the wings and control surfaces, or for the bending deformations of the
wings. Qualitatively, the computed flow is as expected, although quantitative
comparisons with the original Flyer cannot be made due to the geometric
details that were omitted.
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Weight with pilot |
750 pounds (339
Kg) |
|
Wing span |
40’ 4“ (12.3 m) |
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Wing chord length |
6.5 ft (2 m) |
|
Engine |
12HP (8950 W) (when hot, at
1090 RPM), 4 cylinders, watercooled, 179 pounds (81 Kg) |
|
Cruise airspeed |
30 MPH (48 KPH) |
|
Stall speed |
25 MPH (40 KPH) |
|
Wings |
spruce ribs and spars cold rolled
steel fittings |
|
Fabric |
Pride of the West muslin, possibly
treated with potato starch and wax |
|
Fuselage truss |
spruce, Douglas fir |
|
Chord Reynolds # |
1.8 million |
Some interesting technical data for the 1903 Wright
Flyer; notice how close the stall speed is to the cruise speed!
More Information
www.centennialofflight.gov
www.ensight.com/news/wrightbros.html
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