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It is known that SEA is a rapid and simple methodology for analyzing complex vibroacoustic systems. However, the SEA principle is not always valid and one has to be careful about the physical conditions at which the SEA principle is acceptable. In this study, the appropriate damping loss factor of the vehicle interior cavity is studied in the viewpoint of the modal overlap factor of the cavity and the decay per mean free path (DMFP) of the cavity. Virtual SEA tests are performed with an FE model combination, which is suggested by a previous study of Stelzer et al. for the simulation of the sound transmission loss (STL) of vehicle panel structure. The FE model combination is consisting of the body in white (BIW), an acoustical-excited hemisphere-shaped exterior cavity, and the interior cavity. It is found that the DMFP of the interior cavity is appropriate between 0.5 ~ 1 dB for applying SEA principle.

Aerodynamic simulation results are most of the time compared to wind tunnel results. It is too often simplistically believed that it suffice to take the CAD geometry of a car, prepare and run a CFD simulation to obtain results that should be comparable. With the industry requesting accuracies of a few drag counts when comparing CFD to wind tunnel results, a careful analysis of the element susceptible of creating a difference in the results is in order. In this project a detailed 1:4 scale model of the Hyundai Genesis was tested in the model wind tunnel of the FKFS. Five different underbody panel configurations of the car were tested going from a fully paneled car to a car without panels. The impact of the moving versus static ground was also tested, providing over all ten different experimental results for this car model.

Cryopreservation of the biological sample usually requires rapid cooling in order to suppress the growth of intracellular ice and to reach the temperature below the vitrification temperature. The ultra-rapid cooling technique by using liquid nitrogen is favorable because it is safe, inexpensive, and harmless in most cases. This paper describes the transient heat transfer phenomena when the object is suddenly plunged into subcooled liquid nitrogen. The heat transfer coefficient in this rapid cooling process is very different from that of the steady state boiling where the quasi-static approximation is made. The cooling experiment used 0.2 mm thick copper disk. The temperature history was precisely measured during cooling process under various subcooled conditions (from 65 K to 77 K) of liquid nitrogen. The data is used not only for analyzing the cooling rate but also for estimating the instantaneous heat transfer coefficients.