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- <h1>Documentation for OpenRocket</h1>
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- <li>OpenRocket</li>
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- <h2>User documentation</h2>
-
- <p>No user's guide currently exists for OpenRocket. There is a
- <a href="http://apps.sourceforge.net/mediawiki/openrocket/index.php?title=User%27s_Guide">page on the wiki</a> for creating a User's guide.</p>
- <p>If you would like to help, please extend it!</p>
-
-
- <h2>Technical documentation</h2>
-
- <p>OpenRocket was originally written as the Master's thesis of
- Sampo Niskanen at Helsinki University of Technology. The thesis
- currently functions as the technical documentation, and will be
- updated in the future to account for further enhancements.
- The thesis is licensed under a
- <a rel="license" href="http://creativecommons.org/licenses/by-nd-nc/1.0/fi/deed.en">Creative Commons BY-NC-ND License</a>.</p>
-
- <p class="right"><a rel="license" href="http://creativecommons.org/licenses/by-nd-nc/1.0/fi/deed.en"><img alt="Creative Commons BY-NC-ND License" src="http://i.creativecommons.org/l/by-nd-nc/1.0/fi/88x31.png" /></a></p>
-
-
-
- <p><a href="thesis.pdf">Development of an Open Source model
- rocket simulation software</a> (PDF, 1.3MB)</p>
-
-
- <p class="quote"><strong>Table of contents:</strong></p>
- <ol class="toc">
- <li>1. Introduction</li>
- <li>2. Basics of model rocket flight</li>
- <li>3. Aerodynamic properties of model rockets</li>
- <li>4. Flight simulation</li>
- <li>5. The OpenRocket simulation software</li>
- <li>6. Comparison with experimental data</li>
- <li>7. Conclusion</li>
- </ol>
- <ol class="toc">
- <li>A. Nose cone and transition geometries</li>
- <li>B. Transonic wave drag of nose cones</li>
- <li>C. Streamer drag coefficient estimation</li>
- </ol>
-
-
- <h2>Resources</h2>
-
- <p>Below are resources that have been found useful in the analysis
- of model rockets. Many useful scientific aerodynamic articles and
- documents are available at the invaluable
- <a href="http://ntrs.nasa.gov/">NASA Technical Resources Server
- (NTRS)</a>.</p>
-
- <dl>
- <dt><em>
- <a href="http://www.apogeerockets.com/Education/downloads/barrowman_report.pdf">The Theoretical Prediction of the Center of
- Pressure</a></em>, James and Judith Barrowman, 1966.</dt>
- <dd>The original NARAM R&D report explaining how to
- calculate the CP position of a rocket.</dd>
-
- <dt><em>
- <a href="http://ntrs.nasa.gov/search.jsp?Ntk=all&Ntx=mode+matchall&Ntt=Barrowman+Practical+Calculation+of+the+Aerodynamic+Characteristics+of+Slender+Finned+Vehicles">The Practical Calculation of the Aerodynamic
- Characteristics of Slender Finned Vehicles</a></em>, James
- Barrowman, 1967.</dt>
- <dd>The more in-depth and technical thesis, where Barrowman
- presents methods for calculating the CP position of a rocket at
- both subsonic and supersonic velocities and its other
- aerodynamic properties. Available on
- <a href="http://ntrs.nasa.gov/">NTRS</a>.</dd>
-
- <dt><em>
- <a href="http://projetosulfos.if.sc.usp.br/artigos/sentinel39-galejs.pdf">Wind instability—What Barrowman left out</a></em>,
- Robert Galejs.</dt>
- <dd>An extension to the Barrowman method to account for body
- lift at large angles of attack.</dd>
-
- <dt><em>Topics in Advanced Model Rocketry</em>, Mandell,
- Caporaso, Bengen, MIT Press, 1973.</dt>
- <dd>An excellent theoretical study on the flight of model
- rockets. Available as a reprint edition.</dd>
-
- <dt><em>Fluid-dynamic drag</em>, Sighard Hoerner,
- published by the author, 1965.</dt>
- <dd>An excellent resource for all kinds of experimental data
- regarding drag. Available as a reprint edition.</dd>
-
- <dt><em>Tactical missile design</em>, 2nd edition, Eugene
- L. Fleeman, AIAA, 2006.</dt>
- <dd>Useful approximation methods for estimating the aerodynamic
- properties of rockets.</dd>
-
- <dt><em><a href="http://www.aoe.vt.edu/~mason/Mason_f/CAtxtTop.html">Applied
- Computational Aerodynamics</a></em>, William Mason.</dt>
- <dd>An online textbook on computational aerodynamics.</dd>
-
- <dt><em><a href="http://www.combatindex.com/mil_docs/pdf/hdbk/0700/MIL-HDBK-762.pdf">Design of aerodynamically stabilized free rockets</a></em>,
- MIL-HDBK-762, US Army Missile Command, 1990.</dt>
- <dd>Military handbook on the design of rockets, a good resource
- for aerodynamic estimation methods.</dd>
-
- <dt><em>
- <a href="http://www.thrustcurve.org/">ThrustCurve.org</a></em>,
- John Coker.</dt>
- <dd>An excellent resource for model rocket motor thrust curves.</dd>
-
- <dt><em>
- <a href="http://ntrs.nasa.gov/search.jsp?Ntk=all&Ntx=mode+matchall&Ntt=NASA-TN-D-4013">Static stability investigation of a single-stage
- sounding rocket at Mach numbers from 0.60 to 1.20</a></em>, James
- Ferris, NASA-TN-D-4013, 1967.</dt>
- <dt><em>
- <a href="http://ntrs.nasa.gov/search.jsp?Ntk=all&Ntx=mode+matchall&Ntt=NASA-TN-D-4014">Static stability investigation of a sounding-rocket
- vehicle at Mach numbers from 1.50 to 4.63</a></em>, Donald Babb and
- Dennis Fuller, NASA-TN-D-4014, 1967.</dt>
- <dd>Experimental data of a wind tunnel investigation of a
- sounding rocket at subsonic, transonic and supersonic
- velocities. Available on
- <a href="http://ntrs.nasa.gov/">NTRS</a>.</dd>
-
-
-
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