Subjects: TÚNEIS DE VENTO, AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
ABNT
CATALANO, Fernando Martini et al. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016, Anais.. Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics, 2016. . Acesso em: 14 ago. 2024.APA
Catalano, F. M., Abdalla, A. M., Cerón Muñoz, H. D., & Munjulury, R. C. (2016). Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. In . Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics.NLM
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 ago. 14 ]Vancouver
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 ago. 14 ]