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= 1903 Wright Flyer =
= for FlightGear with LaRCsim and the UIUC Aeromodel =
= =
= Michael Selig, et al =
= http://amber.aae.uiuc.edu/~m-selig/apasim.html =
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To run, try:
fgfs --aircraft=wrightFlyer1903-v1-nl-uiuc --enable-auto-coordination --start-date-sys=1903:12:18:10:35:00:
Files and directory structure required in $FG_ROOT/Aircraft/ to fly the
model:
wrightFlyer1903-v1-nl-uiuc-set.xml
wrightFlyer1903/Sounds/uiuc/wrightFlyer1903-sound.xml
UIUC/wrightFlyer1903-v1-nl/aircraft.dat
UIUC/wrightFlyer1903-v1-nl/CDfa.dat
UIUC/wrightFlyer1903-v1-nl/Cmfa2.dat
UIUC/wrightFlyer1903-v1-nl/Cmfade6.dat
UIUC/wrightFlyer1903-v1-nl/CLfade.dat
These files above come with the FlightGear base package.
Files and directory structure required in $FG_ROOT/Aircraft/ to see the
external 3D model
wrightFlyer1903/Models/uiuc/03Flyer/03Flyer.mdl
wrightFlyer1903/Models/uiuc/03Flyer/flywheel.bmp
wrightFlyer1903/Models/uiuc/03Flyer/panel.bmp
wrightFlyer1903/Models/uiuc/03Flyer/pilotook.bmp
wrightFlyer1903/Models/uiuc/03Flyer/sprocket_32.bmp
wrightFlyer1903/Models/uiuc/03Flyer/wing2_32.bmp
wrightFlyer1903/Models/uiuc/03Flyer/wing2.bmp
wrightFlyer1903/Models/uiuc/03Flyer/03Flyer-model.xml
Information on these files can be obtained from Wolfram Kuss' website
here:
http://home.t-online.de/home/Wolfram.Kuss/
The 3D model is here:
http://home.t-online.de/home/Wolfram.Kuss/FGFS1/FGFS1.htm
Another source is apparently:
http://www.flightxpress.de/files/0402/FS2002/Flugzeuge/wright03.zip
Download the zip file and model files in the directory indicated
above. Under linux, the files from zip archive might need to be
renamed to lower case (if they are not already that way). Renaming to
lower case will be necessary if FlightGear crashes when trying to read
the texture files.
To use the new aircraft model and not the default Opus glider, edit the
wrightFlyer1903-v1-nl-uiuc-set.xml file and change the string:
"Aircraft/UIUC/Models/opus/opus-model.xml"
to
"Aircraft/wrightFlyer1903/Models/uiuc/03Flyer/03Flyer-model.xml"
after the model files have been installed.
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Model description and updates:
9/7/02 - Added in Cmo to account for decrease in moment due to biplane effect
5/26/02 - First release: v1-nl
* This model is based partly on wind tunnel tests of a 1903 Wright
Flyer replica tested at NASA Ames by a group lead by Prof Culick at
Caltech. The model is a nonlinear model, meaning that stall is
included. Because the replica was not tested to stall, data in this
regime had to be deduced from a number of different sources,
including low Reynolds number airfoil data taken at UIUC.
* Wonder what it was like to fly the 1903 Wright Flyer? Be a test
pilot. See the longitudinal static instability. Fly steady,
straight and level using some trim to help relieve pressure on the
stick, then put in a brief canard pulse (elevator stick) so as not
to change the trim speed. With an up canard pulse and hands off the
stick, the Wright Flyer will start to pitch upwards until it
stalls. Down pulse, and it goes down. This same instability is seen
by simply trying to fly straight and level! The rates are low
enough that a good pilot with practice can stay ahead of the static
instability. Stall can get pretty nasty if both the canard and
biplane wing stall at the same time. Typically, however, only the
canard will stall first. Full up elevator can be used to fly out of
the dive. But in this condition the canard is stalled. Relieving
the back pressure will move the canard out of stall and the pull-out
will be a little bit faster, but the difference is hard to notice.
Keep in mind that this aircraft was flown four times before it was
damaged on Dec 17, 1903. The first flight was 120 feet in 12
seconds, and the last was 852 feet in 59 seconds. How far can you
fly?
* Run with the FGFS "enable-auto-coordination" option (see run command
at the top of this file) to model the coupling between the wing
warping and rudder to counteract the adverse yaw effect of the wing
warping. The amount of coupling has been tuned to match that on the
original Wright Flyer. The resulting handling is not that great.
For later designs, the Wright Brothers decoupled the warping and
rudder to have more control and the ability to fly in coordinated
flight ("cross-controls").
* Finally, it's a hand full!
* References:
- Culick, F.E.C. and Jex, H.R., "Aerodynamics, Stability and
Control of the 1903 Wright Flyer," Proceedings of The Wright
Flyer: An Engineering Perspective, National Air and Space Museum,
Smithsonian Institution, 1985.
- Jex, H.R. and Culick, F.E.C., "Flight Control Dynamics of the
1903 Wright Flyer," 12th AIAA Atmospheric Flight Mechanics
Conference, AIAA Paper 85-1804-CP, 1985.
- Jex, H, Grimm, R., Latz, J.P., and Hange, C., "Full-Scale 1903
Wright Flyer Wind Tunnel Test Results From the NASA Ames Research
Center", AIAA 38th Aerospace Sciences Meeting, AIAA Paper
2000-0512, 2000.
- Various other sources including
http://www.wrightflyer.org/Papers/papers.html
http://amber.aae.uiuc.edu/~m-selig/uiuc_lsat.html (low Re data)
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
**************************************************
Prof. Michael S. Selig
Dept. of Aerospace Engineering
University of Illinois at Urbana-Champaign
306 Talbot Laboratory
104 South Wright Street
Urbana, IL 61801-2935
(217) 244-5757 (o), (509) 691-1373 (fax)
m-selig@uiuc.edu
http://www.uiuc.edu/~m-selig
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