Computational Mechanics Research and Support for Aerodynamics ...
Computational Mechanics Research and Support for Aerodynamics ...
Computational Mechanics Research and Support for Aerodynamics ...
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Figure 2.36: Comparison of velocity uni<strong>for</strong>mity along different sections<br />
Figure 2.37 shows the cross-sectional velocity contour at the potential testing section in the main<br />
channel. Figure 2.37(a) is the result from a smoothly curved trumpet, while Figure 2.37(b) is from a<br />
multi-linear trumpet. It illustrates that the “streamlined” version of the trumpet design produces a more<br />
uni<strong>for</strong>m velocity distribution than the multi-linear one does along a long stretch of the straight channel<br />
downstream.<br />
TRACC/TFHRC Y2Q2 Page 55