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2015 SAE Aero Design East Team

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Presentation on theme: "2015 SAE Aero Design East Team"— Presentation transcript:

1 2015 SAE Aero Design East Team
Group Status Report

2 SAE Aero East 2015 Team Project Advisor Dr. Drew Landman Team Leader
Jeremy Newman Team Members Andrew Tonkovic Mason Hunerkoch Chris Thurman Michael Lauruska Greg Shively Ryan Laporte Kevin Rhamy Sara Mendelsohn Lucas Mills William Fisher

3 Overview Project Schedule Project Budget Competition Technology Report
Construction Progress Test Flights Future Work Conclusion

4 Project Schedule

5 Project Budget Actual parts cost ≈ $1600
Budgeted Parts Cost = $ Able to reuse some parts and materials from 2014 project

6 Competition Technology Report
30 page technology report submitted January 26 Contains calculations, drawings and experimental data Graphs: Payload prediction Up to 29.5 lbf Structural analysis Von Mises Stress =1.43 ksi Max. vert. displacement = inches Lift vs. Drag Lift vs. Angle of Attack (AOA)

7 Construction Progress
Truss Fuselage Motor mount Wing tail section Nose cone Gussets and ply sections for the fuselage Tail section/fuselage integration Wing/fuselage integration Main Wheel Fabrication Monokote fuselage and wing

8 Wing/Fuselage Monokote

9 Main Wheel/Landing Gear

10 Wing Comparison 2015 Wing 2014 Wing Weight (lbf): 2.406 Span (in): 94
Chord (in): 17 Planform area (in2): 1598 Weight (lbf): Span (in): 84 Chord (in): 15 Planform area (in2): 1260

11 Aircraft Mock-up

12 Test Flights Initial Test Flight
Vibrations induced by the motor did not excite natural frequencies of the motor mount Triple tail tested successfully Distance between tail and wing section tested successfully

13 Test Flights Secondary Test Flight
Rudder control surface proved insufficient Telemetry unit collected flight data Adequate Take-off distance (< 200ft) Sustained flight in high wind conditions ( mph)

14 Test Flights Max. Max. Elevation ≈ 276 ft Speed ≈ 46 mph Take-Off

15 Future Work Test flight(s) final aircraft Flight data collection
Make adjustments based on test flights Resize rudder control surface Competition logistics Competition PowerPoint Document: Competition results Lessons learned

16 Questions?


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