2012
DOI: 10.3329/jname.v9i2.12567
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Numerical simulations of flow past an autonomous underwater vehicle at various drift angles

Abstract: Three dimensional (3D) flow past an Autonomous Underwater Vehicle (AUV) is simulated using a Computational Fluid Dynamics (CFD) approach at a Reynolds (Re) number of 2.09*10 6 . A nonlinear k-ε (NLKE) turbulence model is used for solving the Reynolds Averaged Navier-Stokes equations (RANSE). The effect of control surfaces over the flow, the flow interaction between hull and appendages at various Angles of Attack (AoA) and the effect of the symmetry plane is studied. Flow structure, variation of flow variables … Show more

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Cited by 4 publications
(2 citation statements)
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“…Many numerical studies have been carried out to simulate the flow around the AUVs with a variety of methods. [16][17][18] The nature of complex vertical flow structures around the axisymmetric body with two different nose shapes (SUBOFF and DRDC STR) was experimentally investigated. Results indicated the nose curvature effects on the separation position, and also nose separation for the model with blunter nose shape takes place in smaller incidence angles.…”
Section: Introductionmentioning
confidence: 99%
“…Many numerical studies have been carried out to simulate the flow around the AUVs with a variety of methods. [16][17][18] The nature of complex vertical flow structures around the axisymmetric body with two different nose shapes (SUBOFF and DRDC STR) was experimentally investigated. Results indicated the nose curvature effects on the separation position, and also nose separation for the model with blunter nose shape takes place in smaller incidence angles.…”
Section: Introductionmentioning
confidence: 99%
“…Also, the separation point moved towards the nose at higher angle of attack. Gomatam et al (2012) conducted extensive numerical computations to study the effects of variations in drift angle on the flow past AUVs. The study showed that the presence of the control surfaces and non-zero angles of attack cause nonlinearity in pressure variation at the downstream of the axisymmetric body.…”
Section: Introductionmentioning
confidence: 99%