Grid fins provide good maneuverability to missiles in supersonic flow because they can maintain lift at a higher angle of attack. Although static aerodynamic data exist, very little quantitative dynamic performance information is available for grid fin controlled missiles. The high drag associated with grid fins is also a concern. Dynamic simulations are carried out using computational fluid dynamics to investigate the dynamic stability of a generic missile, controlled by grid fins or planar fins, in supersonic and transonic regimes at angles of attack up to 30 deg. In supersonic flow, the pitch-damping derivative is found to be insensitive to the control fin type; however, in transonic flow, grid fins provide a lower damping in pitch than planar fins due to the blockage effect induced by its choked cells. The reduction of the high drag associated with grid fins is also investigated by comparing the performances of two isolated grid fin geometries with and without the use of a Busemann biplane configuration. The application of this concept to grid fins reduces its drag in the supersonic regime while maintaining its beneficial lift characteristics. Furthermore, the drag of grid fins in transonic flow can be reduced by using an optimized profile with a higher inletto-throat area ratio.
is an open access repository that collects the work of Arts et Métiers ParisTech researchers and makes it freely available over the web where possible.This is an author-deposited version published in: https://sam.ensam.eu Handle ID: .http://hdl.handle.net/10985/8454 To cite this version :Antoine DESPEYROUX, Abdelhak AMBARI, Abderrahim BEN RICHOU -Wall effects on the transportation of a cylindrical particle in power-law fluids -Journal of Non-Newtonian Fluid Mechanics -Vol. 166, n°19-20, p.1173-1182 -2011 Any correspondence concerning this service should be sent to the repository b s t r a c tThe present work deals with the numerical calculation of the Stokes-type drag undergone by a cylindrical particle perpendicularly to its axis in a power-law fluid. In unbounded medium, as all data are not available yet, we provide a numerical solution for the pseudoplastic fluid. Indeed, the Stokes-type solution exists because the Stokes' paradox does not take place anymore. We show a high sensitivity of the solution to the confinement, and the appearance of the inertia in the proximity of the Newtonian case, where the Stokes' paradox takes place. For unbounded medium, avoiding these traps, we show that the drag is zero for Newtonian and dilatant fluids. But in the bounded one, the Stokes-type regime is recovered for Newtonian and dilatant fluids. We give also a physical explanation of this effect which is due to the reduction of the hydrodynamic screen length, for pseudoplastic fluids. Once the solution of the unbounded medium has been obtained, we give a solution for the confined medium numerically and asymptotically. We also highlight the consequence of the confinement and the backflow on the settling velocity of a fiber perpendicularly to its axis in a slit. Using the dynamic mesh technique, we give the actual transportation velocity in a power-law ''Poiseuille flow'', versus the confinement parameter and the fluidity index, induced by the hydrodynamic interactions.
In this paper a new method is presented in order to determine the pore size distribution in a porous media. This original technique uses the non Newtonian yield-pseudo-plastic rheological properties of some fluid flowing through the porous sample. In a first approximation, the very well-known and simple Carman-Kozeny model for porous media is considered. However, despite the use of such a huge simplification, the analysis of the geometry still remains an interesting problem. Then, the pore size distribution can be obtained from the measurement of the total flow rate as a function of the imposed pressure gradient. Using some yield-pseudo-plastic fluid, the mathematical processing of experimental data should give an insight of the pore-size distribution of the studied porous material. The present technique was successfully tested analytically and numerically for classical pore size distributions such as the Gaussian and the bimodal distributions using Bingham or Casson fluids (the technique was also successfully extended to Herschel-Bulkley fluids but the results are not presented in this paper). The simplicity and the cheapness of this method are also its assets.
In non-Newtonian fluids, the mass or heat transfer on particles are of major interest in many industrial processes using suspensions such as fluidized beds or microfluidics reactors. In all these problems we often face hydrodynamic and mass or thermal interactions between a single particle and others or between a single particle and some walls. In this study, such confined configurations can be modeled by a spherical particle translating parallel to the axis of a cylindrical tube. As the suspending fluid may be non-Newtonian, and before examining any possible additional viscoelastic effect on suspension, the first step in the understanding of the consequences of the principal non-Newtonian behavior is the study of the shear thickening or shear thinning (power law model) regarding the transfer phenomena. Then, when the particle translates along the axis of the tube in symmetrical configuration, we numerically solved the momentum and mass (or heat) transfer equations using the stream/vorticity functions formulation coupled to the singularity technique in order to make a numerical conformal mapping for the mesh. For Newtonian fluids, the successful comparisons firstly between our numerical results and asymptotical solutions obtained by us in the lubrication regime, and secondly between our results and those obtained by other authors in unlimited medium, confirm the validity of our approach. Thereby we extended this method to power law fluids. As the geometrical distribution of particles in suspensions is not at all symmetric, we study the influence of some geometrical disturbance breaking the symmetry of the system. To answer this question, we numerically investigate, using the finite volume method, the simple configuration of single spherical particles translating parallel to and in the off-axis position in the tube.
Grid fins have found different applications over the last three decades, from control surfaces in missiles and projectiles to emergency brakes and stabilization devices in space vehicles. Particularly, lattice fins provide a higher maneuverability to agile high-speed missiles in supersonic flow due to their capacity to maintain lift at higher angles of attack, while improving yaw and roll stability. The aerodynamic data available for such configurations includes static aerodynamic coefficients and stability derivatives, but there is only scarce information concerning dynamic stability derivatives such as the pitch damping derivative. Dynamic simulations have been carried out using the Stanford University Unstructured (SU 2 ) CFD code to investigate dynamic stability and maneuverability properties of a grid fin tail controlled generic missile in supersonic (Ma = 2) and transonic regimes (Ma = 0.9) at angles of attack up to 30˚. The pitch damping derivative is shown to be independent from the type of fin in supersonic regime whereas grid fins provide a lower damping in pitch than planar fins in transonic regime. The high drag generated by grid fins is also investigated numerically in this work. The Busemann biplane concept is applied to lattice fins and is shown to reduce significantly their drag in supersonic regime while maintaining their lift characteristics. The high drag in transonic flow can be reduced by using an "optimized Busemann" profile having a higher inlet-to-throat area ratio.
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