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<!DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 4.01 Transitional//EN" "http://www.w3c.org/TR/1999/REC-html401-19991224/loose.dtd">
<HTML xmlns="http://www.w3.org/1999/xhtml">
<HEAD>
<TITLE>JSBSim Open Source Flight Dynamics Model</TITLE>
<META http-equiv=Content-Type content="text/html; charset=windows-1252">
<META content="JSBSim, flight simulation, fdm, flight dynamics, equations of motion" name=keywords>
<LINK media=screen href="StyleSheet2.css" type=text/css rel=stylesheet>
<META content="MSHTML 6.00.6000.16674" name=GENERATOR></HEAD>
<BODY>
<DIV id=topTitle align=left>
<DIV id=redBlockText>An <EM>open source</EM>,<BR>platform-independent,<BR>flight dynamics & control software library in C++
</DIV>
</DIV>
<UL class=solidblockmenu>
<LI><A href="index.html">Home</A></LI>
<LI><A href="about.html">About Us</A></LI>
<LI><A href="https://github.com/JSBSim-Team/jsbsim/releases">Download</A></LI>
<LI><A href="documentation.html" title="JSBSim reference material">Documentation</A></li>
<LI><A class="current" href="links.html">Links</A></LI>
<LI><A href="https://github.com/JSBSim-Team/jsbsim">GitHub/JSBSim</A></LI>
<LI><A href="https://github.com/JSBSim-Team/jsbsim/discussions" title="Ask a question to the JSBSim team.">Support Requests</A></LI>
<LI><A href="https://github.com/JSBSim-Team/jsbsim/issues" title="View or file a bug report.">Issues</A></LI>
<LI><A href="https://github.com/JSBSim-Team/jsbsim/wiki">Wiki</A> </LI>
<LI><A href="aeromatic2.html" title="Generate aircraft configurations files.">Aeromatic</A></LI>
<LI><A href="matlab.html" title="Use JSBSim with MATLAB/Simulink">MATLAB</A></LI>
</UL>
<DIV id=main align=center>
<DIV id=mainText>
<DIV align=left>
<TABLE cellSpacing=0 cellPadding=0 width="100%" border=0>
<TBODY>
<TR>
<TD width="1%"> </TD>
<TD colSpan=2>
<P><STRONG>Links</STRONG><BR>
<BR>The following links are provided solely because they may
feature information useful to aircraft flight simulation modelers.
</P>
<P><U>Table of Contents</U></P>
<UL>
<LI>
<A href="links.html#general">
General Links</A></LI>
<LI>
<A href="links.html#opensource">
Open Source Software Tools</A></LI>
<LI>
<A href="links.html#onlinebooks">
Online Books, References, and Tutorials</A></LI>
<LI>
<A href="links.html#importantnasaaiaa">
Important NASA & AIAA Reports</A><BR/>
- Simulation<BR/>
- Aircraft Modeling Data</LI>
<LI>
<A href="links.html#importantnaca">
Important Historical NACA Reports<BR/></A>
- Propellers<BR/>
- Helicopters<BR/>
- Aircraft Performance<BR/>
- Mass Properties<BR/>
- Aerodynamics</LI>
<LI>
<A href="links.html#onlineperiodicals">
Aerospace Periodicals</A></LI>
</UL>
<P>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle useMap="" border=0>
This symbol denotes a key JSBSim development resource.<BR/><BR/>
<A href="index.html" target=_top>
Back to the JSBSim homepage</A><br/>
</P>
</TD></TR>
<TR>
<TD width=1> </TD>
<TD style="text-align:left">
<A name="general"/>
<P><STRONG>General</STRONG></P>
<UL>
<LI><A href="http://flightgear.sourceforge.net/">
FlightGear Home Page</A></LI>
<LI><A href="http://techreports.larc.nasa.gov/cgi-bin/NTRS">
NASA Langley Technical Report Server</A></LI>
<LI><A href="http://www.pdas.com/">
Public Domain Aeronautical Software*</A></LI>
<LI><A href="http://www.gamasutra.com/">
GamaSutra Game Developer's Site</A></LI>
<LI><A href="http://www.opengl.org/">
OpenGL</A></LI>
<LI><A href="http://www.microwings.com/">
MicroWings</A></LI>
<LI><A href="http://www.airforce-technology.com/index.html">
Air Force Technology</A></LI>
<LI><A href="http://aviation-safety.net/database/type/">
Aviation Safety: Sorted by Aircraft Type</A></LI>
<LI><A href="http://www.ae.uiuc.edu/m-selig/">
UIUC Applied Aerodynamics Group</A></LI>
</UL>
<A name="opensource"/>
<P><STRONG>Open Source Software Tools We Use</STRONG></P>
<UL>
<LI>
<A href="http://www.stack.nl/~dimitri/doxygen/">
Doxygen - Automatic generation of API documentation</A></LI>
<LI>
<A href="http://www.cygwin.com/">Cygwin - A Unix-like environment under MS Windows
</A></LI>
<LI>
<A href="http://www.cvshome.org/">CVS</A> -
"Concurrent Versions System", code management software</LI>
</UL>
<A name="onlinebooks"/>
<P><STRONG>Online Books, References, and Tutorials</STRONG></P>
<UL>
<LI>
<A href="http://adg.stanford.edu/aa208/amsc.html">
Aerodynamic Modeling for Simulation and Control</A></LI>
<LI>
<A href="http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/MainFrame?OpenFrameSet">
FAA: Type Certificate Data Sheets</A></LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/mcfarland.html">
NASA: "Real-Time Simulation Documents"</A></LI>
<LI>
<A href="http://history.nasa.gov/SP-367/cover367.htm">
NASA SP-367: "Introduction to the Aerodynamics of Flight"</A></LI>
<LI>
<A href="http://history.nasa.gov/SP-09-511.pdf">
NASA SP-09-511: "Celebrating a Century of Flight"</A></LI>
<LI>
<A href="http://history.nasa.gov/centtimeline/index.html">
NASA: "The First Century of Flight: NACA/NASA Contribution to Aeronautics"</A></LI>
<LI>
<A href="http://www.hq.nasa.gov/office/pao/History/SP-60/cover.html">
NASA SP-60: "X-15 Research Results"</A></LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://www.movesinstitute.org/~zyda/pubs/Presence.1.4.pdf">
NPSNET: Flight Simulation Dynamic Modeling Using Quaternions</A></LI>
<LI>
<A href="http://www.aoe.vt.edu/~mason/Mason_f/MRsoft.html">
Virginia Tech, Dr. William Mason: Software for Aerodynamics and Aircraft
Design</A></LI>
<LI>
<A href="http://www.aoe.vt.edu/~mason/Mason_f/MRedumatl.html">
Virginia Tech, Dr. William Mason: Electronic Course Materials</A></LI>
</UL>
<A name="importantnasaaiaa"/>
<P><STRONG>Important & Relevant NASA & AIAA Reports</STRONG></P>
<P><U><STRONG>Simulation</STRONG></U></P>
<UL>
<LI>
<A href="http://daveml.nasa.gov/papers/DAVEusingXML.pdf">
Flight Dynamic Model Exchange using XML</A> (Adobe PDF)</LI>
<LI>
<a href="http://hdl.handle.net/2060/20040110806">
Architecting a Simulation Framework for Model Rehosting</a>(Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19990046064">
Design and Development of Lateral Flight Director, NASA/TM-1999-208957</A> (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/20040034718">
Simulating the ARES Aircraft in the Mars Environment</A> (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/20040085931">
Rapid Prototyping of an Aircraft Model in an Object-Oriented Simulation</A> (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19910009766">
Simple Dynamic Engine Model for Use in a Real-Time Aircraft Simulation With Thrust Vectoring</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.nasa.gov/centers/dryden/pdf/88238main_H-1731.pdf">
MODELING, SIMULATION, AND FLIGHT CHARACTERISTICS OF AN
AIRCRAFT DESIGNED TO FLY AT 100,000 FEET, NASA-TM-104236, September
1991, DFRC</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.nasa.gov/centers/dryden/pdf/88059main_H-1356.pdf">
SIMULATION STUDIES OF ALTERNATE LONGITUDINAL CONTROL
SYSTEMS FOR THE SPACE SHUTTLE ORBITER IN THE LANDING REGIME,
NASA-TM-86815, January 1986, DFRC</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.nasa.gov/centers/dryden/pdf/88241main_H-1741.pdf">
A SIMULATION EVALUATION OF A FOUR-ENGINE JET TRANSPORT
USING ENGINE THRUST MODULATION FOR FLIGHTPATH CONTROL, NASA-TM-4324,
September 1991, DFRC</A> (Adobe PDF)</LI>
<LI>
<A href="http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920003846_1992003846.pdf">
An Aircraft Model for the AIAA Controls Design Challenge</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Delays.pdf">
Analyzing Time Delays in a Flight Simulation Environment
AIAA-90-3174, Sept. 1990</A> (Adobe PDF)</LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Basis.pdf">
A Standard Kinematic Model for Flight Simulation at
NASA-Ames NASA CR 2497, Jan. 1975</A> (Adobe PDF)<BR/>
Note: Equation 3.27 in this reference (CR2497) is in error.
The equation should be:
<PRE>Phidot = P + [Q*sin(phi) + R*cos(phi)] * [sin(tht)/cos(tht)] </PRE>
For comparison,
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Toms.pdf">
see Simulator Aero Model Implementation NASA Ref. Pub. 1374,
DOT/FAA/CT-94/83</A> or Stevens and Lewis "Aircraft Control and
Simulation" second edition, eqn. 1.3-22a.</LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Toms.pdf">
Simulator Aero Model Implementation NASA Ref. Pub. 1373,
DOT/FAA/CT-94/83, 1995</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/NRev.pdf">
The N/Rev phenomenon in Simulating a Blade-Element Rotor
System NASA TM 84344, March 1983</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/shock.pdf">
Anticipation of the Landing Shock NASA TM 89465, Sept.
1987</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Feast.pdf">
Finite Element Aircraft Simulation of Turbulence NASA TM
110437, Feb. 1997</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/Sorbet.pdf">
Simulation of Rotor Blade Element Turbulence NASA TM
108862, Jan. 1995</A> (Adobe PDF)</LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13
alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://www.movesinstitute.org/~zyda/pubs/Presence.1.4.pdf">
NPSNET: Flight Simulation Dynamic Modeling
Using Quaternions</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.simlabs.arc.nasa.gov/library/mcfarland/trim.pdf">
Trimming an Aircraft Model for Flight Simulation NASA TM
89466, OCT. 1987</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.ae.uiuc.edu/m-selig/apasim/pubs/AIAA_Paper_2003-0023.pdf">
Icing Encounter Flight Simulator</A> (Adobe PDF)</LI>
<LI>
<A href="http://www.nasa.gov/centers/dryden/pdf/88104main_H-1391.pdf">
Derivation and Definition of a Linear Aircraft Model</A> (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19880020435">
Minimum-complexity helicopter simulation math model</A> (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19940031931">
The Analysis of a Generic Air-to-Air Missile
Simulation Model</A> NASA-94-TM109057 (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19950019882">
Aerodynamics Model for a Generic ASTOVL Lift-Fan
Aircraft</A> NASA Technical Memorandum 110347 (Adobe PDF)</LI>
<LI>
<A href="http://www.nasa.gov/centers/dryden/pdf/88087main_H-1394.pdf">
Aircraft Parameter Estimation</A> AIAA Dryden Lecture in Research for 1987,
NASA Technical Memorandum 88281 (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19790011963">
Stability and Control Derivative Estimates Obtained
From Flight Data for the Beech 99 Aircraft</A>
NASA Technical Memorandum 72863 (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19950012150">
In-Flight Lift-Drag Characteristics for a
Forward-Swept Wing Aircraft (and Comparisons With Contemporary
Aircraft)</A> NASA Technical Paper 3414 (Adobe PDF)</LI>
<LI>
<A href="http://hdl.handle.net/2060/19930022544">
Supersonic Aerodynamic Characteristics of an
Advanced F-16 Derivative Aircraft Configuration</A>
NASA Technical Paper 3355 (Adobe PDF)</LI>
<LI>
<A href="http://www.holycows.net/datcom/AIAA-1985-4070-141.pdf">Prediction of
Fighter Aircraft Dynamic Derivatives Using Digital DATCOM</A>, Blake,
1985 (409 KB Adobe PDF)</LI>
</UL>
<P><U><STRONG>Aircraft Modeling Data</STRONG></U></P>
<UL>
<LI>
<A href="NASA_CR-96008.pdf">
Aircraft Stability and Control Data</A>
, G. Teper, 1969, NASA CR-96008 (3.2 MB Adobe PDF) Aircraft
presented: A-7A, A-4D, F-104, F-105B, B-58, Navion, DC-8</LI>
<LI>
<A href="NASA_TN_D-5361.pdf">
Analysis Of Lateral-Directional Stability Characteristics Of A Twin-Jet Fighter
Airplane At High Angles Of Attack</A>, Chambers, Anglin, 1969, NASA TN
D-5361 (5.0 MB Adobe PDF) Aircraft Presented: F-4 Phantom (extensive
data presented)</LI>
<LI>
<A href="NASA_TN_D-6993.pdf">
Summary of Directional
Divergence Characteristics of Several High-Performance Aircraft
Configurations</A>, Greer, 1972, NASA TN D-6993 (3.4 MB Adobe PDF)
Aircraft Presented: X-15, F-104, F-4, F-111, F-5/T-38, B-58, etc.</LI>
<LI>
<A href="NASA_CR-2144.pdf">Aircraft Handling
Qualities Data</A>, Heffley, Jewell, 1972, NASA CR-2144 (6.9 MB Adobe
PDF) Aircraft Presented: NT-33, F-104A, F-4C, X-15, HL-10, Jetstar,
CV-880, B-747, C-5A, XB-70A Note: This is a key and often-referenced
paper in flight modeling - a real gem.</LI>
<LI>
<A href="http://jsbsim.sf.net/NASA_TM-4356.pdf">
Linearized Aerodynamic
and Control Models of the X-29A Airplane and Comparison with Flight
Data</A>, Bosworth, 1992 (3.0 MB Adobe PDF)</LI>
</UL>
<A name="importantnaca"/>
<P><STRONG>Important & Relevant Historical NACA Reports</STRONG></P>
<P><STRONG><U>Propellers</U></STRONG></P>
<UL>
<LI><A href="http://hdl.handle.net/2060/19930081532">
A generalized vortex theory of the screw propeller and its application</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1954/naca-tn-3228/">
Aerodynamic investigation of a four-blade propeller operating through an
angle-of-attack range from 0 to 180 degrees</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1951/naca-tn-2164/">
Axial-momentum theory for propellers in compressible flow</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1948/naca-tn-1721/">
Calculation of the effect of thrust-axis inclination on propeller disk
loading and comparison with flight measurements</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1954/naca-tn-3304/">
Investigation of the aerodynamic characteristics of a model wing-propeller combination and
of the wing and propeller separately at angles of attack up to 90 degrees</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1922/naca-tn-91/">
Notes on propeller design I the energy losses of the propeller</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1920/naca-tm-1/">
On the elementary relation between pitch, slip, and propulsive efficiency</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1926/naca-tn-237/">
Propeller design - a simple system based on model propeller test data III</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1926/naca-tn-236/">
Propeller design extension of test data on a family of model
propellers by means of the modified blade element theory II</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1926/naca-tn-235/">
Propeller design I practical application of the blade element theory</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1922/naca-tm-79/">
Propeller theory of Professor Joukowski and his pupils</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1947/naca-tn-1338/">
Propeller-efficiency charts for light airplanes</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1953/naca-tn-2966/">
Propeller-performance charts for transport airplanes</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1943/naca-wr-l-336/">
Proposal for a propeller side-force factor</A></LI>
<LI>
<IMG style="WIDTH: 26px; HEIGHT: 13px" height=13 alt="This is a key JSBSim development document" hspace=2
src="important.gif" width=26 align=middle border=0>
<A href="http://naca.larc.nasa.gov/reports/1938/naca-report-640/">
The aerodynamic characteristics of full-scale propellers having 2, 3, and 4 blades of
Clark y and R.A.F. 6 airfoil sections</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1922/naca-tn-83/">
The theory of the screw propeller</A></LI>
</UL>
<P><STRONG><U>Helicopters</U></STRONG></P>
<UL>
<LI><A href="http://naca.larc.nasa.gov/reports/1956/naca-report-1266/">
Charts for estimating performance of high-performance helicopters</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1947/naca-tn-1192/">
Charts showing relations among primary aerodynamic variables
for helicopter-performance estimation</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1920/naca-tn-4/">
The problem of the helicopter</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1949/naca-tn-1812/">
The application of airfoil studies to helicopter rotor design</A></LI>
</UL>
<P><STRONG><U>Aircraft Performance</U></STRONG></P>
<UL>
<LI><A href="http://naca.larc.nasa.gov/reports/1929/naca-tn-302/">
A new method for the prediction of airplane performance</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1938/naca-tn-643/">
A study of flying-boat take-off</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1927/naca-tn-257/">
Technical preparation of the airplane - Spirit of St. Louis.</A></LI>
<LI><A href="http://jsbsim.sourceforge.net/spit_flying.pdf">
NACA Report L-334, Measurements of the Flying Qualities of
the Supermarine Spitfire V A Airplane</A></LI>
<LI><A href="http://jsbsim.sourceforge.net/spit_stalling.pdf">
NACA Report L-353, Stalling Characteristics of the Supermarine Spitfire V A
Airplane</A></LI>
</UL>
<P><STRONG><U>Mass Properties</U></STRONG></P>
<UL>
<LI><A href="http://naca.larc.nasa.gov/reports/1936/naca-tn-575/">
Estimation of moments of inertia of airplanes from design data</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1940/naca-tn-780/">
Measured moments of inertia of 32 airplanes</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1953/naca-rm-53b19/">
Weight bar charts</A></LI>
</UL>
<P><STRONG><U>Aerodynamics</U></STRONG></P>
<UL>
<LI><A href="http://naca.larc.nasa.gov/reports/1925/naca-tn-223/">
Determination of the lift and drag characteristics of an airplane in flight</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1952/naca-rm-a52c04/">
Experimental investigation of the static aerodynamic and dynamic damping-in-roll
characteristics of an 8-cm aircraft rocket with solid and slotted
fins</A></LI>
<LI><A href="http://techreports.larc.nasa.gov/ltrs/PDF/NASA-96-tm110216.pdf">
F-18 Simulation</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1922/naca-tn-92/">
Full scale determination of the lift and drag of a seaplane</A></LI>
<LI><A href="http://www.dfrc.nasa.gov/DTRS/1994/PDF/H-1913.pdf">
In-Flight Lift-Drag Characteristics</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1938/naca-tn-666/">
Longitudinal stability in relation to the use of an automatic pilot</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1922/naca-tn-113/">
Report on the general design of commercial aircraft</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1932/naca-tn-412/">
The aerodynamic characteristics of airfoils at negative angles of attack</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1927/naca-tn-269/">
The distribution of loads between the wings of a biplane having decalage</A></LI>
<LI><A href="http://naca.larc.nasa.gov/reports/1938/naca-tn-636/">
The estimation of the rate of change of yawing moment with sideslip</A></LI>
</UL>
<A name="onlineperiodicals"/>
<P><STRONG>Aerospace Periodicals and Online Presence</STRONG></P>
<UL>
<LI>
<A href="http://www.aerospaceonline.com/content/homepage/default.asp?VNETCOOKIE=NO">
Aerospace Online</A></LI>
<LI>
<A href="http://www.aviationnow.com/">
Aviation Week and Space Technology</A></LI>
</UL>
</TD>
<TD width="1%"> </TD></TR>
<TR>
<TD width="1%"> </TD>
<TD>
<UL>
<LI>Thanks to Ralph Carmichael for his support
of the FlightGear project. At <A href="http://www.pdas.com/">Public Domain
Aeronautical Software</A> you will find
the PDAS CD-ROM for sale, packed with great programs of use to
aeronautical engineers. At this web site there are also some sample
downloads to show what is on the CD.</LI>
</UL>
</TD>
<TD> </TD>
<TD width="1%"> </TD></TR></TBODY></TABLE>
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