SAE Aero Design Group 10 Dimitrios Arnaoutis Alessandro Cuomo

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Presentation transcript:

SAE Aero Design Group 10 Dimitrios Arnaoutis Alessandro Cuomo Gustavo Krupa Jordan Taligoski David Williams

Motivation SAE Collegiate Design Series

Project Specifications (rules) Aircraft Dimension Requirement Fully configured for takeoff, the free standing aircraft shall have a maximum combined length, width, and height of 225 inches. Aircraft exceeding this design requirement will be disqualified from the competition. Gross Weight Limit Regular Class aircraft may not weigh more than fifty five (55) pounds with payload and fuel. Engine Requirements Regular Class aircraft can still be powered by a single, unmodified O.S 61FX with

Design Concept – 1 Standard design http://www.uwindsor.ca/aero/system/files/plane.jpg http://www.airliners.net/aviation-forums/non_aviation/print.main?id=1323590

Design Concept – 2 “Flying Wing” http://www.af.mil/shared/media/photodb/photos/030922-F-0000J-888.jpg

Design Concept – 3 Minimalist design http://aerodesign.meil.pw.edu.pl/ad_new/wp-content/uploads/2011/03/IMG_6904na_strone.jpg

Design Concept – 4 Double Wing http://my.fit.edu/cargoplane/img/taxi1%20011.jpg Double Wing

Design Concept – 5 Biplane http://iignite.com/SAE/Gallery/content/bin/images/large/_0114022654.jpg http://www.engin.umich.edu/teamprojects/teams/aero/teamprojects/teams/aero/mfly4.jpg

Materials Carbon Fiber Advanced composites Balsa wood/heat shrink skin http://dsgperformance.files.wordpress.com/2010/03/carbon-fiber-frame-lg.jpg Carbon Fiber Advanced composites Balsa wood/heat shrink skin http://www.airfieldmodels.com/gallery_of_models/rc/wermachts_scorpion/images/17581.jpg

Decision Matrix

Conclusion and Future Plans

References ANY QUESTIONS? Page Reference 2 http://students.sae.org/competitions/aerodesign/east/ 3 4 5 6 7 8 9 ANY QUESTIONS?