Flutter Analysis Model 1.0

Operating systemsOS : Windows / Linux / BSD / Solaris
Program licensingScript Licensing : Freeware
CreatedCreated : Jul 31, 2007
Size downloadDownloads : 7
Program licensing
Thank you for voting...

This model demonstrates how to implement a coupled ...

This model demonstrates how to implement a coupled structural-aerodynamic problem.
The wing, otherwise rigid, is allowed to pitch and plunge. The motion of the wing is defined using simmechanics blocks. The aerodynamic model is a simple, quasi-steady formulation.
Dynamic pressure is manipulated by varying the Mach number & Altitude. You can also vary the CG location of the wing by double clicking on the picture of the BACT subsystem.
The structural, mass, and aerodynamic properties all come from the following paper:
AIAA 96-3437
"Modeling the Benchmark Active Control technology Wind Tunnel Model for Application to Flutter Suppression" by Martin R. Waszak of NASA Langley.
Automatic flutter detection is implemented via a state-machine in Stateflow.
Demands:
aerospace Blockset
• Aerospace toolbox
• SimMechanics
• Simulink
• Stateflow
• Virtual Reality Toolbox

Flutter Analysis Model 1.0 scripting tags: aerodynamic, model, flutter analysis, analysis model, simmechanics, technology, toolbox, aerospace, flutter analysis model, matlab aerospace. What is new in Flutter Analysis Model 1.0 software script? - Unable to find Flutter Analysis Model 1.0 news. What is improvements are expecting? Newly-made Flutter Analysis Model 1.1 will be downloaded from here. You may download directly. Please write the reviews of the Flutter Analysis Model. License limitations are unspecified.