Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.

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Presentation transcript:

Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie

 Plane weight less than 12 lbs (aim for 8)  15 lbs static paylod  Instrumentation package  3 lb expellable payload .45 ci max engine displacement

 GOE 525 airfoil ◦ High Camber ◦ Max Cl/Cd of 74 at 1.75 aoa and 25 mph  Aspect Ratio of 10 ◦ 10’ span with 1’ chord ModelAspect Ratio Wright Flyer6.4 Boeing SAE Aero10 U-214.3

 Wings: 2.25 lb (Both Wings)  Fuselage: 2.75 lb  Tail: 1.25 lb  Fittings/Small Parts: 1 lb  Total: Approx lb  Not Included: Wing bottom and fuselage monokoat, wire extensions, instrumentation

 Parasitic Drag Coefficient: 0.03  Oswald Efficiency Factor: 0.9  Propeller Efficiency: 0.9

 Glide Angle: 4.8 degrees  Glide Range: ft above ground

 Turning Radius (30 mph): 53.8 ft  Angular Velocity (30 mph): 47 degrees/sec

 Control Surface Actuation  Engine Fuel Consumption  Static Thrust  Radio Range Test  Taxi Testing  Ground Effect Flight  Take-Off Roll  In-Flight Stability  In-Flight Control