A Student Developed Sizing Methodology for Electric Powered Aircraft Applied to Small UAVs 2000-01-5536
A sizing methodology for electric-powered aircraft is described. Results of two student design projects which used this methodology are presented. The projects showed that the methodology is useful in obtaining aircraft of minimum size for the performance and payload required.
Citation: Smith, J., Batish, P., Brandt, S., and Morton, S., "A Student Developed Sizing Methodology for Electric Powered Aircraft Applied to Small UAVs," SAE Technical Paper 2000-01-5536, 2000, https://doi.org/10.4271/2000-01-5536. Download Citation
Author(s):
Jonathan R. Smith, Paul G. Batish, Steven A. Brandt, Scott A. Morton
Affiliated:
Department of Aeronautics, USAF Academy
Pages: 8
Event:
World Aviation Congress & Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
Auto/Oil Air Quality Improvement Research Program, Volume Ii-SP-1000
Related Topics:
Electric aircraft
Aircraft
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »
