Camber effects in cascade-gust interaction noise through a simple extension of analytical models
Author:
Affiliation:
1. Airbus
2. University of Sherbrooke
3. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2307
Reference22 articles.
1. On a uniformly valid analytical rectilinear cascade response function
2. On sound generation by the interaction between turbulence and a cascade of airfoils with non-uniform mean flow
3. Amiet,R.K.Highfrequencythin-airfoiltheoryforsubsonicflow.AIAAJournal,Vol.14,pp.1076-1082,1976.
4. THE RESPONSE OF A SWEPT BLADE ROW TO A THREE-DIMENSIONAL GUST
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