Ground effect on tandem flapping wings hovering

DOI10.1016/j.compfluid.2017.04.006zbMath1390.76627OpenAlexW2606668365MaRDI QIDQ1648307

N. G. Srinidhi, S. Vengadesan

Publication date: 27 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2017.04.006

zbMATH Keywords

ground effectIBMdragonflytandem wings

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Finite difference methods applied to problems in fluid mechanics (76M20) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Biopropulsion in water and in air (76Z10)

Related Items (2)

Investigation of the Unsteady Aerodynamics of Insect Flight: The Use of Immersed Boundary Method ⋮ Effects of flapping deviation on the hovering performance of tandem pitching-plunging foils

Uses Software

• PETSc

Cites Work

• Numerical simulation of an oscillating cylinder in a cross-flow at low Reynolds number: forced and free oscillations
• Flight force production by flapping insect wings in inclined stroke plane kinematics
• A cartesian grid method for modeling multiple moving objects in 2D incompressible viscous flow.
• A numerical study on the free hovering flight of a model insect at low Reynolds number
• An adaptive version of the immersed boundary method
• Flow characteristics of two in-phase oscillating cylinders in side-by-side arrangement
• The immersed boundary method: a projection approach
• An immersed interface method for simulating the interaction of a fluid with moving boundaries
• A CFD-informed quasi-steady model of flapping-wing aerodynamics
• IMMERSED BOUNDARY METHODS
• A hybrid immersed-boundary and multi-block lattice Boltzmann method for simulating fluid and moving-boundaries interactions
• Laminar flow past a rotating circular cylinder
• Flow past a rotating cylinder
• Vortex shedding and frequency selection in flapping flight
• Insect normal hovering flight in ground effect
• Aerodynamic properties of a wing performing unsteady rotational motions at low Reynolds number

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