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Aircraft Design 2 – Stability calculation with AVL - ITLiMS

Aircraft Design 2 – Stability calculation with AVL - ITLiMS

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The Faculty of Power and Aeronautical Engineering of Warsw Uniwersity of Technology <strong>–</strong> <strong>Aircraft</strong> <strong>Design</strong> Department<br />

Project 6 <strong>–</strong> Longitudinal static stability and control<br />

Program <strong>AVL</strong> for aerodynamic and aircraft dynamic stability, originaly written by Mr.<br />

Mark Drela and Mr. Harold Youngren, is available free on GPL license on web page:<br />

http://web.mit.edu/drela/Public/web/avl/. Although, the program has text user interface and<br />

simple graphics, it demonstrated it’s usefulness and is still improved and updated. Model<br />

sailplanes designed <strong>with</strong> use of <strong>AVL</strong> can be seen on:<br />

http://www.charlesriverrc.org/articles.htm.<br />

Students should download from the page:<br />

- Binary version of the program appropriate for the system they use, example:<br />

avl327.zip (name of the downloaded file may change <strong>with</strong> the versions). After<br />

unpacking the program is ready to use <strong>with</strong>out any installation.<br />

- Text documentation for <strong>AVL</strong> avl_doc.txt, which contains detailed description of <strong>AVL</strong><br />

functionality.<br />

- Short tutorials session1.txt and session2.txt. It is strongly recommended to go through<br />

this tutorial to get familiar <strong>with</strong> the software.<br />

- Files <strong>with</strong> run cases runs/ directory, which contain example geometry of planes, mass<br />

distributions, flight conditions (run files) and other.<br />

Unpack <strong>AVL</strong> in desired work directory. Get familiar <strong>with</strong> the software by going<br />

through tutorials using example geometry and mass files. Modify example files to suite<br />

geometry and mass distribution of your airplane and save it under new name. Make<br />

aerodynamic and dynamic flight analyses for cruise conditions. Show computed dynamic<br />

stability eigenvalues. If plane is unstable, modify geometry or mass distribution to stabilize it.<br />

Tips & Trics:<br />

- Reading manual is unavoidable, but it is possible to use <strong>AVL</strong> efficiently after one day<br />

of learning.<br />

- If you start <strong>AVL</strong> from script or shell you will be able to read why it crashed even if it<br />

crashed.<br />

- Read what is displayed on screen, it might tell you about your mistakes.<br />

- After opening program “LOAD” some geometry otherwise <strong>AVL</strong> won’t let you do<br />

anything else.<br />

- Type “?” to get list of available commands.<br />

- Modifying example files is butter than building your own from the beginning. This<br />

let’s you avoid mistakes in the text files.<br />

- Make small changes in the text files and control many times if you are still able to load<br />

them. Make backup of files from time to time.<br />

- Pay attention to units. It is advised to use SI units: meters and kilograms.<br />

Jacek Mieloszyk <strong>–</strong> Project Guide: Longitudinal static stability and control 1/2


The Faculty of Power and Aeronautical Engineering of Warsw Uniwersity of Technology <strong>–</strong> <strong>Aircraft</strong> <strong>Design</strong> Department<br />

Requirements:<br />

Aerodynamic analysis (OPER)<br />

o Plot of geometry <strong>with</strong> pressure loads<br />

o List of aerodynamic derivatives<br />

o Neutral point in percents of MAC<br />

Jacek Mieloszyk <strong>–</strong> Project Guide: Longitudinal static stability and control 2/2

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