技术资料
白皮书和应用说明
Evaluation of Novel Wing Design for UAV
发布日期 2014
Viable design alternative for the existing and fast growing UAVs which are optimized for unmanned flight is of great demand. Designing of a small scale UAV alternative to the AAI Aerosonde UAV has been considered changing the wing tail configuration of the vehicle analyzing both structural and aerodynamic performance improvements using COMSOL Multiphysics® software.
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- bahumanyam_presentation.pdf - 1.08MB
- bahumanyam_paper.pdf - 0.75MB
- bahumanyam_abstract.pdf - 0.32MB