Published online by Cambridge University Press: 28 March 2017
A semi-empirical model is presented that describes the development of a fully developed turbulent boundary layer in the presence of surface roughness with length scale   $k_{s}$  that varies with streamwise distance
 $k_{s}$  that varies with streamwise distance   $x$ . Interest is centred on flows for which all terms of the von Kármán integral relation, including the ratio of outer velocity to friction velocity
 $x$ . Interest is centred on flows for which all terms of the von Kármán integral relation, including the ratio of outer velocity to friction velocity   $U_{\infty }^{+}\equiv U_{\infty }/u_{\unicode[STIX]{x1D70F}}$ , are streamwise constant. For
 $U_{\infty }^{+}\equiv U_{\infty }/u_{\unicode[STIX]{x1D70F}}$ , are streamwise constant. For   $Re_{x}$  assumed large, use is made of a simple log-wake model of the local turbulent mean-velocity profile that contains a standard mean-velocity correction for the asymptotic fully rough regime and with assumed constant parameter values. It is then shown that, for a general power-law external velocity variation
 $Re_{x}$  assumed large, use is made of a simple log-wake model of the local turbulent mean-velocity profile that contains a standard mean-velocity correction for the asymptotic fully rough regime and with assumed constant parameter values. It is then shown that, for a general power-law external velocity variation   $U_{\infty }\sim x^{m}$ , all measures of the boundary-layer thickness must be proportional to
 $U_{\infty }\sim x^{m}$ , all measures of the boundary-layer thickness must be proportional to   $x$  and that the surface sand-grain roughness scale variation must be the linear form
 $x$  and that the surface sand-grain roughness scale variation must be the linear form   $k_{s}(x)=\unicode[STIX]{x1D6FC}x$ , where
 $k_{s}(x)=\unicode[STIX]{x1D6FC}x$ , where   $x$  is the distance from the boundary layer of zero thickness and
 $x$  is the distance from the boundary layer of zero thickness and   $\unicode[STIX]{x1D6FC}$  is a dimensionless constant. This is shown to give a two-parameter
 $\unicode[STIX]{x1D6FC}$  is a dimensionless constant. This is shown to give a two-parameter   $(m,\unicode[STIX]{x1D6FC})$  family of solutions, for which
 $(m,\unicode[STIX]{x1D6FC})$  family of solutions, for which   $U_{\infty }^{+}$  (or equivalently
 $U_{\infty }^{+}$  (or equivalently   $C_{f}$ ) and boundary-layer thicknesses can be simply calculated. These correspond to perfectly self-similar boundary-layer growth in the streamwise direction with similarity variable
 $C_{f}$ ) and boundary-layer thicknesses can be simply calculated. These correspond to perfectly self-similar boundary-layer growth in the streamwise direction with similarity variable   $z/(\unicode[STIX]{x1D6FC}x)$ , where
 $z/(\unicode[STIX]{x1D6FC}x)$ , where   $z$  is the wall-normal coordinate. Results from this model over a range of
 $z$  is the wall-normal coordinate. Results from this model over a range of   $\unicode[STIX]{x1D6FC}$  are discussed for several cases, including the zero-pressure-gradient (
 $\unicode[STIX]{x1D6FC}$  are discussed for several cases, including the zero-pressure-gradient (  $m=0$ ) and sink-flow (
 $m=0$ ) and sink-flow (  $m=-1$ ) boundary layers. Trends observed in the model are supported by wall-modelled large-eddy simulation of the zero-pressure-gradient case for
 $m=-1$ ) boundary layers. Trends observed in the model are supported by wall-modelled large-eddy simulation of the zero-pressure-gradient case for   $Re_{x}$  in the range
 $Re_{x}$  in the range   $10^{8}{-}10^{10}$  and for four values of
 $10^{8}{-}10^{10}$  and for four values of   $\unicode[STIX]{x1D6FC}$ . Linear streamwise growth of the displacement, momentum and nominal boundary-layer thicknesses is confirmed, while, for each
 $\unicode[STIX]{x1D6FC}$ . Linear streamwise growth of the displacement, momentum and nominal boundary-layer thicknesses is confirmed, while, for each   $\unicode[STIX]{x1D6FC}$ , the mean-velocity profiles and streamwise turbulent variances are found to collapse reasonably well onto
 $\unicode[STIX]{x1D6FC}$ , the mean-velocity profiles and streamwise turbulent variances are found to collapse reasonably well onto   $z/(\unicode[STIX]{x1D6FC}x)$ . For given
 $z/(\unicode[STIX]{x1D6FC}x)$ . For given   $\unicode[STIX]{x1D6FC}$ , calculations of
 $\unicode[STIX]{x1D6FC}$ , calculations of   $U_{\infty }^{+}$  obtained from large-eddy simulations are streamwise constant and independent of
 $U_{\infty }^{+}$  obtained from large-eddy simulations are streamwise constant and independent of   $Re_{x}$  when this is large. The present results suggest that, in the sense that
 $Re_{x}$  when this is large. The present results suggest that, in the sense that   $U_{\infty }^{+}(\unicode[STIX]{x1D6FC},m)$  is constant, these flows can be interpreted as the fully rough limit for boundary layers in the presence of small-scale linear roughness.
 $U_{\infty }^{+}(\unicode[STIX]{x1D6FC},m)$  is constant, these flows can be interpreted as the fully rough limit for boundary layers in the presence of small-scale linear roughness.
Present address: Mechanical Engineering, Physical Sciences and Engineering Division, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia, 23955-6900.