Society of Automotive Engineers (SAE) Aero Design Team members: - - PowerPoint PPT Presentation

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Society of Automotive Engineers (SAE) Aero Design Team members: - - PowerPoint PPT Presentation

Society of Automotive Engineers (SAE) Aero Design Team members: Saood Alazmi Conor Rich Ahmad Almuhanna Lucas Veteto Michael Torres Faculty Advisor: Dr. David Trevas Acknowledgements Our Sponsors Special thanks to: Dr. David Trevas


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Society of Automotive Engineers (SAE) Aero Design

Team members:

Saood Alazmi Conor Rich Ahmad Almuhanna Lucas Veteto Michael Torres Faculty Advisor:

  • Dr. David Trevas
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Acknowledgements

Special thanks to: Our Sponsors

  • Dr. David Trevas

Alex Klausenstock

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  • The SAE Aero Design competition is designed to provide exposure to real-world challenges professional

engineers encounter in the industry.

  • High percentage of competition points awarded to design report and presentation to emphasize written

and oral skills.

  • The purpose of this competition is to design and construct a remote control (RC) airplane following the

strict requirements of SAE.

  • The R/C airplane has to carry the largest payload while keeping the empty weight low. It will use tennis

balls as “passengers” and half pound weights to represent the “luggage”.

Project Description

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Competition Objectives

  • Design and construct an R/C airplane following the requirements given by the competition.
  • Provide a technical report and 2-D drawing of the final airplane design.
  • Give an oral presentation to the judges.
  • Load the airplane with a ½ pound weight for each tennis ball.
  • Demonstrate the plane’s ability to takeoff, fly in a loop, and land.
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Project Goals and SAE Requirements

  • Project goals:

○ Successfully take off and maintain flight while carrying passenger (tennis balls). ○ Limitations on electric motor power output, battery size, wing construction, etc. ○ Aircraft before loading must be less than 55 lbs.

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  • High coefficient of lift airfoil.

○ Sokolov-il

  • Wing shape changed from tapered to square.
  • Boxed main spar, with bass wood ribs, followed by balsa

paneling, followed by monokote.

○ Basswood vs. Balsa wood vs Plywood

Design Approach: Wings

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Design Approach: Fuselage

  • Solid plywood sides for strength
  • Clear top for competition requirement.
  • A magnetic door on top of the fuselage

○ For wings bolting to the fuselage ○ For access to the aileron servo wiring.

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Design Approach: Nose/Tail

  • Hinged firewall (top)

○ Loading/unloading of passengers and luggage. ○ Attachment point for front landing gear.

  • Removable nose-cone (bottom right)

○ Allows access to electrical component ○ Motor and propellor

  • Tail constructed out of Balsa panels.

○ Control surfaces attached by CA hinges ○ (Bottom Left)

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Design Approach: Payload

  • Separate compartments for passengers and luggage.

○ Tennis balls in upper compartment, luggage in lower. ○ All wiring kept away from passengers and luggage.

  • Tennis balls inserted by sliding tray.
  • Luggage inserted into bottom compartment and bolted in place.
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CAD Design

  • Required for competition
  • Important for design

○ Total weight ○ Center of Gravity (CG)

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  • RISA-2D was used to test the reaction force in the aluminum spar.
  • ~24 lbs of lift generated in each wing. Averaging 4.8 lb/ft of lift along the main spar.
  • Experiences a bending stress of 12,700 psi.

Rod will yield at 35,000 psi.

Factor of Safety = 2.75.

Loading

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Payload Prediction Curve

  • Predicting 21.4 lbs of payload.

○ 4.4 lb tennis balls ○ 17 lb luggage

  • Predicted weight of unloaded plane: 28.8 lb
  • Actual weight of unloaded plane: 31.6 lb
  • Predicted Flight Weight: 50.2 lb
  • Actual total weight: 53 lb
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  • 1st flight attempt

○ Did not fly. ■ Rear wheels were too soft. ■ Loading failure of front landing gear.

Unable to attend competition.

  • 2nd flight attempt

○ Redesign of front and rear landing gear and wheels. ○ Increased the propeller size and pitch. ○ Decreased the wing’s angle of attack. ■ Increased takeoff speed. ■ Crashed on fourth flight.

Results

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Results: Video

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Takeaway

  • Challenges

○ First time group competing against teams with many years of experience ○ Students and Faculty advisor with no aerodynamics experience ○ Limited budget

  • What we learned

○ Calculating the Lift and Drag of a wing ○ Dynamic wing loading ○ Takeoff and landing distances ○ Electronic wiring of remote control aircrafts ○ Practical experience with designing/building

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