Home › Digital Repository › Faculty, Staff and Student Publications/Presentations › Undergraduate Research › Undergraduate Research Day › Undergraduate Research Day 2009 ›
Lockheed Martin/SAE Aero Design Competition
Object Details
View
Title Information
Lockheed Martin/SAE Aero Design Competition
Lockheed Martin/SAE Aero Design Competition
Name:Personal
Mullings, Justin Role :Text(marcrelator)
creator
Mullings, Justin Role :Text(marcrelator)
creator
Name:Personal
Herrera, Angelo Role :Text(marcrelator)
creator
Herrera, Angelo Role :Text(marcrelator)
creator
Name:Personal
Mertes, Christopher Role :Text(marcrelator)
creator
Mertes, Christopher Role :Text(marcrelator)
creator
Name:Personal
Smith, Dr. Doug Role :Text(marcrelator)
contributor
Smith, Dr. Doug Role :Text(marcrelator)
contributor
typeOfResource
still image genre
Origin Information
Place
Laramie, Wyoming
University of Wyoming (keyDate="yes")
2009-05-15
Laramie, Wyoming
University of Wyoming (keyDate="yes")
2009-05-15
Language:Text
eng
eng
Physical Description
born digtal
born digtal
abstract
A heavy-lift, remote-controlled aircraft was designed and fabricated for the 2009 Aero Design competition, which was established by the Society of Automotive Engineers (SAE) and is sponsored by Lockheed Martin. The goal of the aircraft is to lift as much payload as possible within dimensional constraints. The most critical aspect of this project is the design of the wing, which is the most significant contributor of weight to the aircraft, but also must generate enough lift to carry the aircraft along with its payload. Due to the objective of having as low of weight as possible without cargo, the primary aircraft materials consist of polycarbonate, balsa wood, and light-weight aluminum. Mathematical models were developed to describe the behavior of the aircraft during flight in order to predict lifting capabilities, engine thrust, aerodynamic drag, and in-flight stability. Using a highly iterative process, these models were used to develop an appropriate design with payload capabilities of over 25 pounds. The physical components of the aircraft were then configured to conform to competition restrictions and to provide advantageous flight characteristics mirroring those developed with the mathematical models. The fabricated aircraft will be participating in the international Aero Design competition in Marietta, Georgia. note
From - Undergraduate Research Day 2009 - Celebration of Research - Abstracts
Subject
2009 Aero Design
2009 Aero Design
Subject
Society of Automotive Engineers
Society of Automotive Engineers
Subject
Lockheed Martin
Lockheed Martin
Subject
remote-controlled aircraft
remote-controlled aircraft
Related Item:series
Title Information
Undergrauate Research Day 2009
Undergrauate Research Day 2009
Location
(usage="primary display")
accessCondition:useAndReproduction
http://digital.uwyo.edu/copyright.htm
Record Information
languageOfCataloging
:Text(ISO639-2B)
English :Code(ISO639-2B)
eng
English :Code(ISO639-2B)
eng