We use highly resolved numerical simulations to study turbulent Rayleigh-Bénard convection in a cell with sinusoidally rough upper and lower surfaces in two dimensions for P r = 1 and Ra = 4 × 10 6 , 3 × 10 9 . By varying the wavelength λ at a fixed amplitude, we find an optimal wavelength λopt for which the Nusselt-Rayleigh scaling relation is N u − 1 ∝ Ra 0.483 maximizing the heat flux. This is consistent with the upper bound of Goluskin and Doering [1] who prove that N u can grow no faster than O(Ra 1/2 ) as Ra → ∞, and thus the concept that roughness facilitates the attainment of the so-called ultimate regime. Our data nearly achieve the largest growth rate permitted by the bound. When λ λopt and λ λopt, the planar case is recovered, demonstrating how controlling the wall geometry manipulates the interaction between the boundary layers and the core flow. Finally, for each Ra we choose the maximum N u among all λ, and thus optimizing over all λ, to find N uopt − 1 = 0.01 × Ra 0.444 .The ubiquity and importance of thermal convection in many natural and man-made settings is well known [2][3][4]. The simplest scenario that has been used to study the fundamental aspects of thermal convection is the Rayleigh-Bénard system [5]. The flow in this system is governed by three non-dimensional parameters: (1) the Rayleigh number Ra = gα∆T H 3 /νκ, which is the ratio of buoyancy to viscous forces, where g is the acceleration due to gravity, α the thermal expansion coefficient of the fluid, ∆T the temperature difference across a layer of fluid of depth H, ν the kinematic viscosity (or momentum diffusivity) and κ the thermal diffusivity; (2) the Prandtl number, P r = ν/κ; and (3) the aspect ratio of the cell, Γ, defined as the ratio of its width to height.The primary aim of the corpus of studies of turbulent Rayleigh-Bénard convection has been to determine the Nusselt number, N u, defined as the ratio of total heat flux to conductive heat flux (Eq. 1), as a function of the three governing parameters, viz., N u = N u(Ra, P r, Γ). For Ra 1 and fixed P r and Γ, this relation is usually sought in the form of a power law: N u = A(P r, Γ)Ra β , where β has a fundamental significance for the mechanisms underlying the transport of heat.The classical theory of Priestley [6], Malkus [7] and Howard [8] is based on the argument that as Ra → ∞ the dimensional heat flux should become independent of the depth of the cell, resulting in β = 1/3. A consequence of this scaling is that the conductive boundary layers (BLs) at the upper and lower surfaces, which are separated by a well mixed interior, do not interact.However, Kraichnan [9] reasoned that for extremely large Ra the BLs undergo a transition leading to the generation of smaller scales near the boundaries that increase the system's efficiency in transporting the heat, predicting that N u ∼ Ra/ (ln Ra). In this, "KraichnanSpiegel" or "ultimate regime" (β = 1/2), it is argued that the heat flux becomes independent of the molecular properties of the fluid [e.g. and hence values of Ra) t...