Closure to “Computational fluid dynamics for sub-atmospheric pressure analysis in pipe drainage” by Mohsen Besharat, Óscar E. Coronado-Hernández, Vicente S. Fuertes-Miquel, Maria Teresa Viseu and Helena Margarida Ramos, J. Hydraulic Res. 58(4), 2020, 553–565, https://doi.org/10.1080/00221686.2019.1625819

2021 ◽  
Vol 59 (6) ◽  
pp. 1034-1035
Author(s):  
Mohsen Besharat ◽  
Óscar Enrique Coronado-Hernández ◽  
Vicente Samuel Fuertes-Miquel ◽  
Maria Teresa Viseu ◽  
Helena Margarida Ramos
2019 ◽  
Vol 58 (4) ◽  
pp. 553-565 ◽  
Author(s):  
Mohsen Besharat ◽  
Oscar Enrique Coronado-Hernández ◽  
Vicente Samuel Fuertes-Miquel ◽  
Maria Teresa Viseu ◽  
Helena Margarida Ramos

2018 ◽  
Vol 154 ◽  
pp. 01115
Author(s):  
Rahmat Riza ◽  
Dicky Kurniawan ◽  
Arif Budi Wicaksono

NACA0012H is an airfoil type that could be used for Unmanned Aerial Vehicle Medium Altitude Long Endurance. This experiment was used to analyze stress in the surface of Tail of UAV MALE that was caused by air flow. The experiment was conducted using Computational Fluid Dynamics Software. Two designs of tail, horizontal and V-tail, were considered to simulate pressure occurred on the surface of leading edge, chamber and trailing edge. The simulation was developed varying the speed of the UAV MALE. The results showed that pressure occurred on the surface of horizontal tail higher than pressure on the V-tail.


Author(s):  
Juan Carlos Gómez Blanco ◽  
Enrique Mancha Sánchez ◽  
Diego Torrejón Martín ◽  
Juan Pablo Carrasco Amador ◽  
Francisco Miguel Sánchez Margallo ◽  
...  

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