EPSRC Reference: 
EP/I037938/1 
Title: 
Scale Interactions in Wall Turbulence: Old Challenges Tackled with New Perspectives 
Principal Investigator: 
Morrison, Professor J 
Other Investigators: 

Researcher CoInvestigators: 

Project Partners: 

Department: 
Aeronautics 
Organisation: 
Imperial College London 
Scheme: 
Standard Research 
Starts: 
10 July 2012 
Ends: 
09 July 2015 
Value (£): 
412,679

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Panel History: 
Panel Date  Panel Name  Outcome 
01 Sep 2011

Materials,Mechanical and Medical Engineering

Announced


Summary on Grant Application Form 
The need to improve the efficiency of fluidbased systems is now of paramount importance. In experimental aerodynamics, one of the most difficult measurements is an accurate determination of surface friction. Our need to predict it accurately is fundamentally important to the design of efficient systems. Reynolds number similarity is an essential concept in describing the fundamental properties of turbulent wallbounded flow. Unlike the drag coefficient for bluff bodies, that for a turbulent boundary layer continues to decrease indefinitely with increasing Reynolds number because the smallscale motion near the surface is directly affected by viscosity at any Reynolds number. Therefore Reynolds number similarity is very important in design and is a vital tool for the engineer, who, plied with information from either direct numerical simulations or windtunnel tests (or both), may well have to extrapolate over several orders of magnitude in order to estimate quantities such as drag at engineering or even meteorological Reynolds numbers. Perhaps the most wellknown example of Reynolds number similarity is the region of log velocity variation (the log law) found in wallbounded flows which, at sufficiently high Reynolds numbers, exists regardless of the nature of the surface boundary condition or the form of the outer imposed length scale.
In wallbounded flows relevant to practical applications, where the flow is turbulent and the Reynolds number is high, the transport and loss of fluid momentum and energy is not well understood. Consequently, most predictive and modelling methods rely on a variety of assumptions. The two most critical ones are the Law of the Wall (the log law) and Townsend's localequilibrium hypothesis. Both assumptions implicitly assume that large scales in the flow are weak and that they function independently of the small scales. However, this is clearly not true, especially in flows of engineering importance, such as when the surface is rough or when the flow is not in equilibrium. In fact, there is a multiscale interaction, referred to here as an innerouter interaction (IOI), where the large scales influence the dynamics of the small scales and viceversa. These interactions are not well understood and therefore any corrections to the predictive models to include these interactions are essentially achieved through adhoc means.
A better understanding of IOI will help explain the apparent nonuniversality of the constants in the log law and will certainly influence the development of models for both ReynoldsAveraged NavierStokes (RANS) calculation methods, LargeEddy Simulations (LES) and hybrid RANSLES. It will also be useful in the development of models for the control of wall turbulence, complementing knowledge from Direct Numerical Simulations which, we believe, are inherently incomplete owing to the restriction to low Reynolds numbers. Accurate models for prediction and control at realistic Reynolds numbers typical of practical applications will have to address IOI. Researchers working in specific areas of internal roughwall flows, roughwall boundary layers and freestream turbulence effects on boundary layers will also benefit from this fundamental work. All these aspects are abundantly present in a variety of practical applications and natural systems. For example, researchers exploring modelling strategies for practical applications such as oil and naturalgas pipelines, ship hulls and the natural and urban terrains will find the the data obtained from the roughness experiments to be very useful for validation exercises. Similarly, researchers in the area of turbomachinery will find the data from the roughness and freestream turbulence experiments extremely useful.

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