Aero Design Specifications and Performance Analysis
Learn about the detailed specifications and performance analysis of an aircraft design, including weight distribution, airfoil characteristics, drag coefficients, and operational parameters like glide range and turning radius.
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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 Model Wright Flyer Boeing 727 SAE Aero U-2 Model Aspect 6.4 7.1 10 14.3 Aspect Ratio Ratio
Wings: 2.25 lb (Both Wings) Fuselage: 2.75 lb Tail: 1.25 lb Fittings/Small Parts: 1 lb Total: Approx. 7.25 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: 1200 ft @ 100ft 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
