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Investigating the influence of cells with various geometric parameters on the air flow in the channel

This paper experimentally studies the gas flow structure in a longitudinal flow around a honeycomb surface with hexagonal cells of various sizes and depths. The measurements are carried out using the PIV system for the developed flow in a flat channel with the cross-section of 21 × 150 mm and the length of 1000 mm. The flow is visualized, and the velocity and turbulence components are measured in a smooth channel and in the presence of honeycomb surfaces. It has been shown that a boundary layer with high gradient of velocity and turbulent pulsations is formed near the honeycomb.


Introduction
An important direction in the development of the heat transfer theory and aerohydrodynamics is the search for new methods of heat transfer intensification with a minimal growth of hydraulic losses. In this respect, the surfaces with lunar reliefs are illustrative [1,2]. A number of experimental and numerical studies in this field prove great potential of such methods. The honeycomb surfaces considered in this work, used in particular for the purposes of thermal protection of spacecraft elements and as the seals for gas turbines, have a number of similarities to the well vortex generators. This is evidenced by the results of the first experimental studies of the longitudinal flow around the surfaces with honeycomb coatings [3,4]. Data on acoustic damping [5], which helps to reduce friction, gives all the grounds for using such vortex generators as the effective methods for controlling the processes of turbulent transfer. However, due to the lack of detailed experimental information on the flow structure, it is not possible to create an integrated pattern of this complex phenomenon, and therefore its deeper investigation is required. The development of the flow field and turbulent characteristics along the honeycomb surfaces are studied in this paper. It compares data on the averaged and turbulent characteristics of flowing in a channel with honeycombs and with smooth walls.

Experimental setup and measurement methods
The The experimental setup includes all elements of the wind tunnel to form a qualitative flow: prechamber, nozzle and working channel. The detailed description of setup and measurement system is given in [6]. In the present experiments, development of the flow along the entire length of the honeycomb plate is studied at three different velocities: 5, 10 and 20 m/s; in the beginning of the plate with honeycombs, the flow is developed. The measurements are performed using the PIV system.

Experimental results and discussion
The paper presents the results of measurements of longitudinal velocity profiles, longitudinal and transverse pulsations, and shear stresses in a mooth channel and channel with honeycombs. All data are obtained for cross-section at x/h = 6.5 from the beginning of the surface with hexagonal cells. According to experiments, the flow in the vicinity of the honeycomb surface is fundamentally different from the flow around a smooth wall. In the near-wall region of the honeycomb surface, the velocity profile is gentler in comparison with the classical distribution on a smooth wall (Fig. 1a). At the same time, longitudinal and transverse velocity pulsations (Figs. 1b and 1c, respectively) near the honeycomb surface are several times greater than on the smooth surface. A similar tendency exists for distribution of shear stresses across the channel (Fig. 1d) shear stresses along the height, in the channel with cells at distance y/h ~ 0.2, the stresses increase more than 2-3 times. At the same time, a steady tendency to a decrease in transverse velocity pulsations and turbulent shear stresses is observed directly in the near-wall region. Such a complex scenario of the flow development is caused by interaction of the boundary layer with the honeycomb cells. Indeed, the flow around depressions of various shapes (cylindrical cavity [7], hole [8], transverse trench-groove [9], etc.) on the surface leads to formation of a periodic vortex layer behind them. However, we failed to detect the existence of such structures in the present work.
One of the principal differences between the obtained results and experimental data of [3,4] is the absence of the flow slip along the surface with honeycombs, which, according to this data, could reach about 20-30% of the velocity in the flow core.  Distribution of layer form parameter H = δ * / δ ** along the honeycombs with different ratio d/b is shown in Fig. 2 for three flow velocities (coordinate x = 0 corresponds to the beginning of honeycomb region).
In the diagram, value H corresponds to the developed turbulent flow; then, we can observe its increase to the value characteristic of the laminar flow regime (H → 2.7) and subsequent decrease. This behavior of the form parameter is caused, most likely, by the "flattening" of velocity profile with simultaneous increase in turbulence and tangential stresses. It is not possible now to formulate clearly the reasons for such a behavior of local and integral characteristics of the turbulent flow around the surface with honeycombs, primarily because of multifactority and complexity of the aerodynamic structure, and this will require further detailed studies.

Conclusions
The paper presents the results of experimental study of the averaged flow, normal and tangential stresses in gas, flowing with different velocities around the honeycomb surfaces with characteristic cell size of ~ 5 mm and ~ 12 mm. The measurements were performed using the two-component PIV system.
The flow was organized in a flat channel of 21 × 150 × 1000 mm. It has been found that the boundary layer on the surface with hexagonal cells is less filled than on a smooth wall. At the same time, the growth of turbulent pulsations and tangential stresses is observed simultaneously. However, there is no effect of flow sliding relative to the cells.