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SAE Aero Design West 2008SAE Aero Design West 2008
Information SessionInformation Session
What is the SAE competition?What is the SAE competition?
WhoWho
- Undergrad and Grad Students (SAE Members)- Undergrad and Grad Students (SAE Members)
Competition ComponentsCompetition Components- Design Report, Oral Presentation, FlightDesign Report, Oral Presentation, Flight
Classes of CompetitionClasses of Competition- Regular, Open, MicroRegular, Open, Micro
What is the SAE competition?What is the SAE competition?
PilotsPilots
- - Current members of the Academy of Model Aeronautics or the national model aircraft club
Design and FabricationDesign and Fabrication
- - Designed and built by the SAE student members (without direct involvement from professional engineers, radio control model experts, pilots, machinists, or related professionals)
What is the SAE competition?What is the SAE competition?
Original DesignOriginal Design- Original design whose configuration is
conceived by the student team members
- Use of major components such as wings, fuselage, or empennage of existing model aircraft kits is prohibited
DeadlinesDeadlines
For the 2007 Competition (which has For the 2007 Competition (which has passed)passed)
- Registration form and fees: Registration form and fees: Late Late DecemberDecember
- Design Reports, Plans, and Payload Design Reports, Plans, and Payload Prediction Graph: Prediction Graph: Late FebruaryLate February
Faculty AdvisorFaculty Advisor
Each team is expected to have a Faculty Advisor appointed by the university
Faculty Advisors may notnot design, build or repair any part of the plane
Mission RequirementsMission Requirements
TakeoffTakeoff- Point when main wheels leave groundPoint when main wheels leave ground
- Regular Class: 200 ft ZoneRegular Class: 200 ft Zone- Open Class: 100 ft ZoneOpen Class: 100 ft Zone
Time LimitTime Limit- Five (5) minutes to complete successful takeoffFive (5) minutes to complete successful takeoff
The aircraft must remain intact during takeoff!!
Competition Circuit Competition Circuit RequirementsRequirements
At least One At least One 360° circuit of the field
- Each aircraft must fly past departure end of field
- Turn aircraft through 180° of heading
- Fly past approach end of takeoff zone prior to landing
Competition Circuit Competition Circuit RequirementsRequirements
RUNWAY
Departure EndApproach End and Takeoff Zone
180° Turn from Takeoff
= 360° Circuit of Field
Mission RequirementsMission Requirements
LandingLanding
- Touchdown to the point the aircraft stops moving- Regular Class: 400 ft Zone*Regular Class: 400 ft Zone*- Open Class: 200 ft Zone*Open Class: 200 ft Zone*
- Aircraft must remain on the runaway between landing limits to be considered successful landing.
* Rolling-out beyond the landing zone is allowed, provided the aircraft touches-down within the landing zone.
Mission RequirementsMission Requirements
After LandingAfter Landing
- Aircraft must takeoff and land intact to receive points for the flight attempt, with the exception of broken propellers
No Fly ZonesNo Fly Zones- 11stst Violation – Invalid flight attempt (no points) Violation – Invalid flight attempt (no points)- 22ndnd Violation – Disqualification from event Violation – Disqualification from event
Mission RequirementsMission Requirements
Repairs and AlterationsRepairs and Alterations
- Original design of aircraft presented in written and oral reports must be maintained during competition
- Alterations may only be made with the permission of the judges but will result in penalty points
Design ObjectiveDesign Objective
Regular ClassRegular Class
- Design aircraft that can lift as much weight as possible given dual design constraints of power and wing span limits
- Accurately predicting lifting capacity will result in bonus points
- Max aircraft weight of 55 lbs
Design ObjectiveDesign Objective
Regular ClassRegular Class
Flight Score = Raw Weight Score + Prediction Bonus + Empty Payload Bonus
Raw Weight Score = Weight Lifted in pounds × 4
Prediction Bonus = 20 – (predicted payload – actual payload)2
Design ObjectiveDesign Objective
Open ClassOpen Class
- Design aircraft that can lift as much weight as possible given max aircraft weight limit of 55 lbs.
- No wing span limit
Design ObjectiveDesign Objective
Open ClassOpen Class
Flight Score = Raw Weight Score + Prediction Bonus + Zero Payload Bonus + Stopping Bonus (must be in landing zone)
Raw Weight Score = Weight Lifted in pounds x 3
Prediction Bonus = 20 – (predicted payload – actual payload)2
***Open Class aircraft may earn a flat 20-point bonus by performing a flight with zero payload. This bonus will be available during Flight Round 1 only.
Design ObjectiveDesign Objective
Micro ClassMicro Class- The objective of Micro Class is to design
an aircraft that can carry the highest payload fraction possible while simultaneously pursuing the lowest empty weight possible.
- No wing span limit
Design ObjectiveDesign Objective
Micro ClassMicro Class
Flight Score = (10 – EW) x PF x 13
EW = Empty Weight
PF = Payload FractionPW = Payload Weight
PF = PW / (EW + PW)
***No prediction points are available for micro class
Design ReportDesign Report
PurposePurpose
- To convey to judges how you came to conclusion
- Display the aircraft you built is most suited for the competition
Guideline for reportGuideline for report
Design ReportDesign Report
ContentsContents
- Project report (max 30 pages)
- Aircraft plans- Fifteen-minute
technical presentation- Payload prediction
graphs
Final WordsFinal Words
- Aero Design West will be in spring of 2008Aero Design West will be in spring of 2008- SAE will not be holding a 2009 competitionSAE will not be holding a 2009 competition- Rules can be found Rules can be found herehere- Dr. Oh wants students to be working on Dr. Oh wants students to be working on
this during the spring and summer terms this during the spring and summer terms of 2007 (ideal testing conditions)of 2007 (ideal testing conditions)