Airfoil Tones at Moderate Reynolds Number: A Computational Study
17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference)
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ICAS2014_0818: COMPUTATIONAL COMPARATIVE STUDY FOR DESIGN OF LOW REYNOLDS NUMBER AIRFOIL
British Library Conference Proceedings | 2014
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