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In this paper we discuss a method for determining heat transfer behaviour during tests in aerodynamic wind tunnels. The method involves computing the heat power evacuated by the heat exchanger as a function of the cooling airflow drag. Using dimensional analysis techniques, we define a Thermal Efficiency Coefficient (TEC). Systematic tests on three geometrically different types of vehicles show that there is a universal law governing the variation in TEC with cooling airflow drag. By associating the curve for this universal law with the characteristic curve for the heat exchanger alone, we can compute a TEC value for a measured cooling airflow drag value, and thus determine the vehicle's engine cooling performance during aerodynamic tests.

Increasing design emphasis on factors such as styling, fuel reduction and soundproofing raises a number of additional problems concerning under-bonnet aerodynamics and heat exchange. Because experimental work on successive prototypes entails heavy penalties in terms of development lead-time, it is becoming more and more important to integrate simulation from the pilot study stage, as a way to minimize the number of prototypes. Fortunately, early integration of under-bonnet air-flow modelling is becoming an increasingly viable proposition, thanks to the spectacular increase in computer processing power, which stimulates the development of more efficient meshing software and facilitates the generalized implementation of CAD techniques throughout the design processes. Modelling thus emerges as a new investigatory method that enhances the design office's capabilities by enabling it to adopt a sharper design focus right from the pilot project stage.