2020
DOI: 10.1007/978-3-030-37393-1_14
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Conceptual Design and Comparative CFD Analyses on Unmanned Amphibious Vehicle for Crack Detection

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Cited by 23 publications
(18 citation statements)
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“…The aerodynamic flow velocity of 10 m/s based computational results is shown in Figures 10 to 12. In Figure 10, the negative sign of pressure is corresponds for dynamic pressure and the velocity induced by the shape of the UAV is 2.414 m/s [Vijayanandh R et al (2020) and Vijayakumar Mathaiyan et al ( 2011 FR4 based composite is reacted lower than other lightweight materials under aerodynamic load. Thus, the lifetime of this same GFRP composite is quite higher than other lightweight material.…”
Section: Cfd Results -Above the Surface Of Oceansmentioning
confidence: 95%
“…The aerodynamic flow velocity of 10 m/s based computational results is shown in Figures 10 to 12. In Figure 10, the negative sign of pressure is corresponds for dynamic pressure and the velocity induced by the shape of the UAV is 2.414 m/s [Vijayanandh R et al (2020) and Vijayakumar Mathaiyan et al ( 2011 FR4 based composite is reacted lower than other lightweight materials under aerodynamic load. Thus, the lifetime of this same GFRP composite is quite higher than other lightweight material.…”
Section: Cfd Results -Above the Surface Of Oceansmentioning
confidence: 95%
“…After a method was developed for constructing this UAmV, the next major phase comprised domain preparation, discretization, and computational procedure. These phases are based on data from the third literature survey [16][17][18][19][20][21][22]. Since the authors of this current work have predominantly relied on the ANSYS Workbench tool for all kinds of computations, this third sub-section is filtered and focused only on obtaining the boundary and initial conditions relevant for the aforesaid computational set-up.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Since the authors of this current work have predominantly relied on the ANSYS Workbench tool for all kinds of computations, this third sub-section is filtered and focused only on obtaining the boundary and initial conditions relevant for the aforesaid computational set-up. The information about the development of control volume, procedures to develop structural meshes, and procedures to attain reliable outcomes for computational hydrodynamic simulations were obtained [16][17][18][19][20][21][22]. Apart from the primary conditions, the secondary conditions provide significant support in computational fluid dynamic (CFD) simulations.…”
Section: Literature Reviewmentioning
confidence: 99%
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