TY - GEN
T1 - New algorithms for reduced memory and real-time noise prediction
AU - Goldman, Benjamin A.
AU - Brentner, Kenneth S.
PY - 2012
Y1 - 2012
N2 - The past few decades have seen the development of numerous aeroacoustic prediction codes. Algorithms based on the Lighthill acoustic analogy, and the Ffowcs Williams-Hawkings (FW-H) equation in particular, are now widely used in industry to predict the aeroacoustic field generated by aerospace vehicles and non-aerospace machinery. In a trend similar to the growth of cluster computing, the size and scale of aeroacoustic problems being computed with these codes has increased dramatically in recent years. A discussion of different algorithms to reduce memory and enable real-time noise prediction is presented. The results of a new data structure and computation algorithm recently implemented in the aeroacoustic prediction code PSU-WOPWOP are shown to significantly decrease the memory requirements - a useful outcome for large permeable surface computations. Only small changes to the algorithm are required to enable the real-time prediction of helicopter rotor noise.
AB - The past few decades have seen the development of numerous aeroacoustic prediction codes. Algorithms based on the Lighthill acoustic analogy, and the Ffowcs Williams-Hawkings (FW-H) equation in particular, are now widely used in industry to predict the aeroacoustic field generated by aerospace vehicles and non-aerospace machinery. In a trend similar to the growth of cluster computing, the size and scale of aeroacoustic problems being computed with these codes has increased dramatically in recent years. A discussion of different algorithms to reduce memory and enable real-time noise prediction is presented. The results of a new data structure and computation algorithm recently implemented in the aeroacoustic prediction code PSU-WOPWOP are shown to significantly decrease the memory requirements - a useful outcome for large permeable surface computations. Only small changes to the algorithm are required to enable the real-time prediction of helicopter rotor noise.
UR - http://www.scopus.com/inward/record.url?scp=84880581805&partnerID=8YFLogxK
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M3 - Conference contribution
AN - SCOPUS:84880581805
SN - 9781600869327
T3 - 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
BT - 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
T2 - 18th AIAA/CEAS Aeroacoustics Conference 2012 (33rd AIAA Aeroacoustics Conference)
Y2 - 4 June 2012 through 6 June 2012
ER -