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A new Hyundai Aero-acoustic Wind Tunnel (HAWT) has been opened in the Nam-yang Technical Center of Hyundai Motor Company (HMC) since August 1999. This wind tunnel has a 3/4 semi-open jet test section and a closed circuit in order to improve aerodynamic and wind noise and thermodynamic characteristics of vehicles. The HMC technical center had started the feasibility study of full-scale wind tunnel in 1995, to improve the aerodynamic characteristics and to meet fuel consumption regulations. The main purpose of this facility is conduct various kinds of tests on customer driving conditions, including aerodynamic and aero-acoustic tests and engine cooling simulations, etc. The technical specification was made on the basis of HMC engineers' experience of their own model scale and full-scale wind tunnels (like MIRA or DNW) during last 10 years.

In order to reduce total drag during aerodynamic optimization process of the passenger vehicle, induced drag should be minimized and pressure drag should be decreased by means of applying streamlined body shape. The reduction of wake area could decrease pressure drag, which was generated by boundary layer separation. The induced drag caused by rear axle lift and C-pillar vortex can be reduced by the employing of trunk lid edge and kick-up or an optimized rear spoiler. When a rear spoiler or kick-up shape was installed on the rear end of a sedan vehicle, drag was reduced but the wake area became larger. This contradiction cannot be explained by simply using Bernoulli’s principle with equal transit or longer path theory. Newtonian explanation with COANDA effect is adopted to explain this phenomenon. The relationships among COANDA effect, down wash, C-pillar vortex, rear axle lift and induced drag are explained.