The torque associated with overcoming the losses on a rotating disc is of particular importance to the designers of gas turbine engines. Not only does this represent a reduction in useful work, but it also gives rise to unwanted heating of metal surfaces and the adjacent fluid. This article presents a numerical study on the effect of rotor-mounted bolts on the moment coefficient and velocity distributions within a rotor–stator cavity under conditions representative of modern gas turbine engine design. Steady-state, two-dimensional and three-dimensional, computational fluid dynamics simulations are obtained using the FLUENT commercial code with a standard k–ɛ turbulence model. The model is validated against experimental data and then used to investigate the effects of varying the number of bolts and also a continuous ring. Two test cases are investigated: one corresponds to where the flow structure is dominated by the superimposed flow (λT = 0.35); and the other, where rotation is expected to govern the flow structure (λT = 0.35). The principal flow phenomena in the vicinity of the bolts were described using the simulation results. Increasing the number of bolts will decrease the relative total pressure difference around bolts and increase the tangential velocity of the core of fluid between the rotor and stator. It was also found out that the free-stream Reynolds number of the flow approaching the bolts decreases and angle of attack increases with increasing number of bolts. As a consequence, the bolts’ wake character changes leading to a situation where the wake of one bolt is not fully collapsed in advance of the following bolt. The occurrence of Taylor columns were also investigated in the rotor–stator system with rotor-mounted bolts. It was found that while increasing the number of bolts can decrease the Rossby number to produce an intermediate rotation in the system, the Taylor columns will not be produced even for 60 bolts under the both flow conditions. The contribution of skin friction to the overall moment coefficient reduces as the number of bolts increases and the pressure-related losses increase. Increasing the number of bolts will decrease the moment produced by each individual bolt. However, since there are more bolts in the system the total moment of all bolts will increase by increasing their number. There also appears to be a point where increasing the number of bolts does not bring about an increase in the overall moment coefficient. It is also interesting to report that the moment coefficient associated with a continuous ring is similar to that for a plain disc.

This paper presents a numerical study of the effect of rotor mounted bolts on the moment coefficient and flow structure within a rotor-stator cavity representative of modern gas turbine engine design. The CFD computations are performed using the commercial code FLUENT. The simulation methodology is first validated using experimental data from plain co-rotating disc and rotor-stator cavities from the open literature. Comparisons are then made with experimental data obtained from a test rig at the Thermo Fluid Mechanics Research Centre (TFMRC), University of Sussex. Computations were performed at Reφ = 6.8 × 106, Cw = 5929 (λT = 0.35) with different numbers of bolts (0 < N < 60), and also a continuous ring, at r/b = 0.9. The study has improved the current understanding of the effect on moment coefficient and flow structure that rotor mounted protrusions have in rotor-stator systems. It is seen that the contribution of skin friction to the moment coefficient reduces as the number of bolts is increased. The size and shape of the wake created by a rotating bolt also means that the pressure loss per bolt reduces with N but the overall effect is to increase the moment coefficient because there are more bolts.