Fifteen submissions in the tandem cylinders category of the First Workshop on Benchmark problems for Airframe Noise Computations are summarized. Although the geometry is relatively simple, the problem involves complex physics. Researchers employed various block-structured, overset, unstructured and embedded Cartesian grid techniques and considerable computational resources to simulate the flow. The solutions are compared against each other and experimental data from 2 facilities. Overall, the simulations captured the gross features of the flow, but resolving all the details which would be necessary to compute the noise remains challenging. In particular, how to best simulate the effects of the experimental transition strip, and the associated high Reynolds number effects, was unclear. Furthermore, capturing the spanwise variation proved difficult.
Summary of the Tandem Cylinder Solutions from the Benchmark Problems for Airframe Noise Computations-I Workshop
49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition ; 2011 ; Orlando, FL, United States
2011-01-04
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2011
|Emerald Group Publishing | 2001
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