Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.
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Transcript of Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.
![Page 1: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/1.jpg)
EMEC 499 SAE Aero Design
CompetitionCraig Kohring, Pat Tice, Sean Dineen, Mark Gasser
James Pallardy, Katie Schipf, AJ Dayvie
![Page 2: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/2.jpg)
Plane weight less than 12 lbs (aim for 8) 15 lbs static paylod Instrumentation package 3 lb expellable payload .45 ci max engine displacement
Competition Rules Recap
![Page 3: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/3.jpg)
![Page 4: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/4.jpg)
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
Wing Design
Model Aspect Ratio
Wright Flyer 6.4
Boeing 727 7.1
SAE Aero 10
U-2 14.3
![Page 5: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/5.jpg)
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
Weight
![Page 6: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/6.jpg)
Parasitic Drag Coefficient: 0.03
Oswald Efficiency Factor: 0.9
Propeller Efficiency: 0.9
Assumptions
![Page 7: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/7.jpg)
Thrust Required Curve
![Page 8: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/8.jpg)
Power Required Curve
![Page 9: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/9.jpg)
Rate of Climb
![Page 10: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/10.jpg)
At Bozeman
![Page 11: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/11.jpg)
Comparison (Sea Level to Bozeman)
![Page 12: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/12.jpg)
Stability
![Page 13: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/13.jpg)
Glide Angle: 4.8 degrees
Glide Range: 1200 ft @ 100ft above ground
Gliding Flight
![Page 14: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/14.jpg)
Turning Radius (30 mph): 53.8 ft
Angular Velocity (30 mph): 47 degrees/sec
Turning
![Page 15: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/15.jpg)
![Page 16: Craig Kohring, Pat Tice, Sean Dineen, Mark Gasser James Pallardy, Katie Schipf, AJ Dayvie.](https://reader034.fdocuments.us/reader034/viewer/2022042822/56649eb65503460f94bbf6c5/html5/thumbnails/16.jpg)
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
Testing