Turbulent skin friction can be significantly (almost by 50%) reduced by the spanwise oscillations of the wall, as shown in Figure 1.
Fig.1. Directions of the flow and of the wall oscillations
More importantly, the power required to move the wall might be not so large, so that in an ideal case almost 20% of fuel spent on overcoming skin-friction drag can be saved. For this, however, the wall motion has to be quite complicated, with the spanwise wall velocity forming a wave travelling in the main flow direction:
It is hard to imagine an aircraft wing surface performing such a complicated motion. In order to make this method practical one needs to understand the phenomenon, and then to use this understanding for finding a simpler method of actuation.
Linearised Navier-Stokes equations (LNSE) has already proved to be a useful tool in predicting near-wall structures in turbulent flows. Importantly, when developed turbulence is concerned, using LNSE is not based on the assumption of small magnitude of perturbations, as it is usual in other applications of LNSE. In developed turbulence, LNSE arise as a result of rearranging the full nonlinear equations with the LNSE terms on one side all the other terms on the other side. It turns out that as far as many (but not all) properties of the solution are concerned LNSE acts as a filter, so that its output is relatively independent of the form of the input, as far as the input is sufficiently broadband, which is of course the case in turbulent flows. In application to the drag reduction by spanwise oscillations, linearization is done about the phase-averaged mean profile of the turbulent flow. Since LNSE are much simpler than the full equations, they are much easier to understand.
Fig.2. Contour plots over actuation parameter space (ω, k_{x}) of: a) drag reduction as calculated by Quadrio et. al. (2009); b) Percentage change in streak amplification as calculated from LNSE.
Figure 2 shows the comparison between the drag reduction obtained numerically and a related quantity predicted on the basis of LNSE. These results give a hope that actuation methods that are easier to implement in a real aircraft might be developed based on the progress made so far.
Further information:
Note: one can watch the videos directly from the Miscellanious tab, but it is better to download the archived versions.
Try it, it is easy and it is fun!
Studying fluid flows with auxiliary functions and LMIsat the IFAC World Congress, held in Yokohama, Japan on 8-14th July 2023.
Bounding time averages: a road to solving the problem of turbulenceat Institut de Mathématiques de Bordeaux, Bordeaux, May 4, 2023.
Bounding time averagesand
How quasi-steady is the modulation of near-wall turbulence by large-scale structures?(with Yunjiu Yang).
Auxiliary functionals: a path to solving the problem of turbulenceat The Seminar in the Analysis and Methods of PDE (SIAM PDE) on March 4, 2021. Links to the abstract and the video.
Accelerating time averagingat 73rd Annual Meeting of the APS Division of Fluid Dynamics, November 22, 2020: abstract and video.
Accelerating time averaging using auxiliary functionsat the Aerodynamics and Flight Mechanics group seminar, University of Southampton, on 6 February 2019
Coherent structures in wall-bounded turbulence: new directions in a classic problem, London, August 29-31, 2018, with a talk
Large-scale motions for the QSQH theory(with Chi Zhang).
Questions concerning quasi-steady mechanism of the Reynolds number, pressure gradient, and geometry effect on drag reductionat the Workshop on Active Drag Reduction, Aachen, Germany, 15-16 March 2018.
The problem of turbulence: bounding solutions to equations of fluid mechanics & other dynamical systems, with Giovanni Fantuzzi providing exercise sessions, at The 6th Bremen Winter School
Dynamical systems and turbulence, March 12-16, 2018.
Sergei Chernyshenko