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Several race car competitions seek to limit engine power through a rule that requires all of the engine combustion air passes through a hole of prescribed diameter. As the approach and departure wall shapes to this hole, usually termed orifice or restrictor are not prescribed, there is opportunity for innovation in these shapes to obtain maximum flow and therefore power. This paper reports measurements made for a range of restrictor types including venturis with conical inlets and outlets of various angles and the application of slotted throats of the ‘Dall tube’ type. Although normal venturis have been optimized as subsonic flow measuring devices with minimum pressure losses, at the limit the flow in the throat is sonic and the down stream shocks associated with flow transition from sub-sonic to sonic are best handled with sudden angular changes and the boundary layer minimized by the corner slots between the convergent and divergent cones.

This paper presents some of the modelling and experimental work being carried out at the University of Melbourne, in collaboration with CMC Research, on their new Scotch yoke engine concept. It begins with an overview of the engine, its compactness and friction advantages. The development of a one dimensional ‘squeeze film’ model is outlined and some simulation results are presented for both a motored and fired engine. A novel feature of the model is the introduction of an ‘un-filled factor’ to account for the dynamics of the oil film volume particular to this type of linear bearing. Experimental results are presented to highlight the important features and serve as a means of validating the model predictions. Comparisons show that the squeeze model correlates reasonably well with the experimental data and it is concluded that the current, flat, bearing design works by a predominantly squeeze film mechanism.