“…In general, hydrodynamics of water impacting can be demonstrated commendably by scaled model water tank tests. In the case of seaplanes, both hydrodynamics and aerodynamic aspects play the same key roles in the dynamic behavior and there is however a difficulty in achieving the correct scaling for the air and water domains (Duan et al, 2019). Froude ( ) scaling guarantees the correct reproduction of the ratio between the inertia and gravity force in the water domain but it do not allow to preserve the Reynolds ( ) similarity and thus the correct scaling of the viscous effects which are important in both water and, especially, in air for the aerodynamic lift and drag (Terziev et al, 2022;Iafrati and Grizzi, 2019).…”
Section: Introductionmentioning
confidence: 99%
“…The whole process was divided into a number of small time-step, and the forces were calculated at each time step. In (Duan et al, 2019) evaluated the porpoising motion, an unstable oscillation phenomenon that threatens the flying safety of amphibious aircrafts, by using a two-phase flow solver in OpenFOAM. Both slipstream caused by the propeller and external forces, viz.…”
The maximal acceleration is proportional to the square of the initial velocity for the V-shaped body• The theoretical ratio of the corresponding velocity to the initial velocity is valid for large impact velocity • Gravity effect should be considered with slow impact speed • A coupled relation among max , * and * is found
“…In general, hydrodynamics of water impacting can be demonstrated commendably by scaled model water tank tests. In the case of seaplanes, both hydrodynamics and aerodynamic aspects play the same key roles in the dynamic behavior and there is however a difficulty in achieving the correct scaling for the air and water domains (Duan et al, 2019). Froude ( ) scaling guarantees the correct reproduction of the ratio between the inertia and gravity force in the water domain but it do not allow to preserve the Reynolds ( ) similarity and thus the correct scaling of the viscous effects which are important in both water and, especially, in air for the aerodynamic lift and drag (Terziev et al, 2022;Iafrati and Grizzi, 2019).…”
Section: Introductionmentioning
confidence: 99%
“…The whole process was divided into a number of small time-step, and the forces were calculated at each time step. In (Duan et al, 2019) evaluated the porpoising motion, an unstable oscillation phenomenon that threatens the flying safety of amphibious aircrafts, by using a two-phase flow solver in OpenFOAM. Both slipstream caused by the propeller and external forces, viz.…”
The maximal acceleration is proportional to the square of the initial velocity for the V-shaped body• The theoretical ratio of the corresponding velocity to the initial velocity is valid for large impact velocity • Gravity effect should be considered with slow impact speed • A coupled relation among max , * and * is found
“…Studies on this issue have been conducted to predict the total drag of fast ships [11,12]. The other study, Fridsma hull was used for numerical verification of OpenFOAM code in seaplane simulation during takeoff [13].…”
Spray strips are deflectors added to the hull to reduce the Wetted Surface Area (WSA). The reduced WSA will decrease the total ship drag caused by the deflection of the spray strip installation. The research aimed to predict the function of the spray strip to improve ship performance using Computational Fluid Dynamics (CFD). The numerical approach in this study used the Finite Volume Method (FVM) with the RANS (Reynolds-averaged Navier–Stokes) equation to solve fluid dynamics problems. VOF (Volume of Fluid) was used to model the water and air phases. The results of this study indicated that the number of spray strips would have a significant effect compared to without using a spray strip. Spray strips with three strips could reduce the total resistance by 4.9% at Fr 1.78. Spray strips would increase the total resistance value by 2.1% at low speeds. Spray strips were effective for reducing total resistance at Fr > 1 or the planing mode conditions. The total resistance prediction used three suggestion profiles with the best performance to reduce total resistance by 6.0% at Fr 1.78.
“…1), where the 2D water entry model is formulated by the added mass method [4,1,2] or the Wagner theory [5,3]. The traditional procedures had been identified to be less accurate as the numerical methods have fast developed in recent decades, and make it possible to conduct numerical simulations of water-landing of seaplanes [6] and transport airplanes [7,8]. Although a whole-time history of water entry of aircraft can be reproduced, massive computational resources are required and several days of calculations are taken.…”
There is an increasing need to develop a two-dimensional (2D) water entry model including the slamming and transition stages for the 2.5-dimensional (2.5D) method being used on the take-off and water landing of seaplanes, and for the strip theory or 2D+t theory being used on the hull slamming. Motivated
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