1 / 9

The flutter analysis of the JS1 glider

The flutter analysis of the JS1 glider. Pieter S. Rossouw Master’s Degree Student Supervisor: Mr. Attie S. Jonker North-West University (Potchefstroom). Introduction. New composite glider: JS1 Revelation 18 meter wingspan Maximum speed: 290 km/h (V ne ) Designed by Attie Jonker

hartwell
Download Presentation

The flutter analysis of the JS1 glider

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. The flutter analysis of the JS1 glider Pieter S. Rossouw Master’s Degree Student Supervisor: Mr. Attie S. Jonker North-West University (Potchefstroom)

  2. Introduction • New composite glider: JS1 Revelation • 18 meter wingspan • Maximum speed: 290 km/h (Vne) • Designed by Attie Jonker & team • Certify new aircraft • Design diving speed (VD) • 1.2VD = 388.8 km/h = 209.9 knots © CSIR 2006 www.csir.co.za

  3. Problem definition/statement • What is flutter? • Flutter analysis main steps • Modal analysis • Flutter prediction • Flutter flight test • Modal analysis done by • Finite element software • Ground vibration test • JS1 flutter analysis steps: • Modal analysis • Flutter prediction © CSIR 2006 www.csir.co.za

  4. Modal analysis • Ground vibration test @ CSIR • Two glider configurations • Simulate free condition • Excitation with electrodynamic shaker • Response measurement with sensors • Dynamic characteristics are • Natural frequency • Mode shape • Modal damping • What is a mode? • Wing, fin and tailplane modes found © CSIR 2006 www.csir.co.za

  5. Modal analysis (continued) © CSIR 2006 www.csir.co.za

  6. Modal analysis (continued) • 2nd symmetric wing bending @ 7.34 Hz © CSIR 2006 www.csir.co.za

  7. Flutter prediction • Use modal data in flutter code • Flutter code utilizes • Doublet lattice method • p-k method • Flutter results • Damping vs. airspeed • Frequency vs. airspeed • Altitudes up to 8000 meters • One indication of flutter: 430 knots • Results above 210 knots – no concern © CSIR 2006 www.csir.co.za

  8. Flutter prediction (continued) 210 knots (1.2VD) © CSIR 2006 www.csir.co.za

  9. Conclusion • Modal analysis done by • Ground vibration test • Flutter analysis done for • Speeds up to 388.8 km/h (210 knots) • Altitudes up to 8000 meters • For all modes found • Stability for JS1 design envelope © CSIR 2006 www.csir.co.za

More Related