The Design and Development of an Active Smart Wing Wind Tunnel Model

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Presentation transcript:

The Design and Development of an Active Smart Wing Wind Tunnel Model ATAK Technologies

Presentation Outline Team Identification Previous Project Accomplishments Project Objectives Project Deliverables Answer Questions

Team Identification Robert R. Aguirre Vu Tran Thomas Ayers Project Leader Senior Research Specialist Vu Tran Senior Testing Specialist Thomas Ayers Senior Controls Specialist Kevin Mackenzie Senior Modeling and Design Specialist Dr. R. O. Stearman University of Texas Faculty Consultant

Previous Accomplishments Familiarization with aerodynamic theory behind oscillating flaps Studied and decided upon an electric actuation system to drive the flaps Preliminary wing designs Proof of design functionality and frequency requirements through preliminary testing of a continuous rod model wing

Objectives Design an F-18 Wing Model using AUTOCAD Construct operational model Attach model to existing controller system Determine testing procedures in order to gather useful information Test wing model in wind tunnel

Project Deliverables End of Semester Project Presentation Written Report AUTOCAD Design of F-18 Wing model Testing Procedures Testing Results F-18 Oscillating Wing Model Functional Simple Wing Controller

Any Questions?