TY - GEN
T1 - Design of a Delta Wing Aircraft
AU - Perez, Luis Raul Montano
AU - Lara, Miroslava Cano
AU - Rios, Higinio Juarez
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/12/27
Y1 - 2017/12/27
N2 - This work shows a UAV (Unmanned Aerial Vehicle) modeling of a fixed wing type and a delta wing configuration. The selection of an aerodynamic profile and the aircraft dimension was chosen. On a CAD package the geometric design was created, where the finite element analysis and fluid dynamics shows that the behavior of the aircraft follows the parameters required to be functional to manufacture and assemble their components.
AB - This work shows a UAV (Unmanned Aerial Vehicle) modeling of a fixed wing type and a delta wing configuration. The selection of an aerodynamic profile and the aircraft dimension was chosen. On a CAD package the geometric design was created, where the finite element analysis and fluid dynamics shows that the behavior of the aircraft follows the parameters required to be functional to manufacture and assemble their components.
KW - Aerodinamic analysis
KW - Delta wing
KW - Finite element analysis
KW - Fluid dynamics
UR - http://www.scopus.com/inward/record.url?scp=85049236708&partnerID=8YFLogxK
U2 - 10.1109/ICMEAE.2017.26
DO - 10.1109/ICMEAE.2017.26
M3 - Contribución a la conferencia
AN - SCOPUS:85049236708
T3 - Proceedings - 2017 International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2017
SP - 93
EP - 97
BT - Proceedings - 2017 International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2017
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2017
Y2 - 21 November 2017 through 24 November 2017
ER -