Trajectory Optimization of eVTOL and Conventional Aircraft: A Comparative Analysis of Vortex Particle Method and Vortex Lattice + Blade Element Momentum Theory
- Award ID(s):
- 2139551
- PAR ID:
- 10584976
- Publisher / Repository:
- American Institute of Aeronautics and Astronautics
- Date Published:
- ISBN:
- 978-1-62410-716-0
- Format(s):
- Medium: X
- Location:
- Las Vegas, Nevada
- Sponsoring Org:
- National Science Foundation
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