2015 SAE Aero Design East Competition
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Transcript 2015 SAE Aero Design East Competition
2015 SAE Aero Design East
Competition
BATTAGLIA MARIO
FACCIO PEDRO
SALAZAR ANDRES
Faculty Advisor: Dr. Dulikravich
Problem Statement
Design and build a remote control airplane that can
lift as much payload as possible while meeting the
restrictions given by the organizers of the event.
Represent Florida International University in the
SAE Aero Design Series competition.
Design Objectives
Implement numerical analysis and knowledge
acquired in the design process to solve a real-life
challenge.
Research in several aerodynamic designs by
performing wind tunnel testing
Analyze design alternatives based on cost and
manufacturing possibilities
Optimized aircraft to obtain higher efficiency
Regular Class Requirements
Maximum combined length, width, and height of 175
inches.
Aircraft may not weight more than fifty-five pounds
with payload.
The use if Fiber-Reinforced Plastic (FRP) is
prohibited.
Single electrical motor configuration.
Design Evaluation
Phase 1 - Technical Report
Phase 2 - Technical Presentation and Inspection
Payload Loading Demonstration
Payload Unloading Demonstration
Oral Presentation
Phase 3 - Flight Competition
Project Calendar
2015 SAE Aero Design East
Competition Timeline
Resarch
Design
Manufacture Fusilage/Wing/Tail
Assemble of Aircraft
Fly/Test
SAE Report Submision
SAE Presentation
SAE Competition
September
October
November
December
January
10 15 25 5 10 15 20 25 5 10 15 20 25 5 10 15 20 25 5 10 15 20 25
March
13-15
Responsibilities Of each member
Conceptual Design
•
High Wing
•
Conventional Tail
•
Rectangular Wings
Wing Structure
8 ft wingspan.
1 inch aluminum tube
Eppler 423 Airfoil.
Tail Structure
Small tail due to competition parameters.
Balsa ribs and sheeting.
Fuselage Structure
Balsa and Light Ply.
Nose compartment (motor and battery).
Body compartment (competition weight).
Environmental & Economic Aspects
Materials used are recyclable.
No environmental impact.
Materials are relatively inexpensive
Manufacturing is relatively straightforward
Global Learning
Weight carried can represent a high definition
camera, a first aid kit, food, or any small package
that needs to be delivered.
The airplane model can be expanded to mapping or
delivery planes, and our design can be presented to
manufacturers in other countries.
Translation of instructions, used materials, parts,
manufacturing process and units so that our design
can be employed in different areas of the world.
Standards
System-Level Standards:
Design is complaint to SAE Aero Design East 2015
rules and regulations.
Component-Level Standards:
Guidance provided by the SAE on component
usage is followed.