Design of a Micro Aerial Vehicle
PubblicoContenuto scaricabile
open in viewerAn unmanned aerial vehicle was designed and built for the AIAA Design Build Fly 2015 competition. To meet the mission requirements, including speed and weight, the aircraft is designed to have a 10-foot wingspan and 14 inch chord with dihedral and a conventional tail wing configuration. To minimize the weight without durability cost, tubular carbon fiber spars and balsa ribs were used to construct the wings. The 5-foot fuselage consists of bulkheads made from balsa ply connected longitudinally by carbon fiber tubes. An 18 inch diameter propeller driven by a brushless DC motor generates the thrust. The aircraft has a 5 pound payload capability. By combining detailed analysis of aerodynamics, structure, and material with flight test, the team has refined the aircraft design.
- This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
- Creator
- Publisher
- Identifier
- E-project-043015-103527
- Advisor
- Year
- 2015
- Date created
- 2015-04-30
- Resource type
- Major
- Rights statement
Relazioni
- In Collection:
Articoli
Elementi
Thumbnail | Titolo | Visibilità | Embargo Release Date | Azioni |
---|---|---|---|---|
MAV_Final_Report_2015s.pdf | Pubblico | Scaricare |
Permanent link to this page: https://digital.wpi.edu/show/3197xn646