Aeroacoustic validation of the free wake method first on the basis of a H145 main rotor in descent flight

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ERF2016_155_P. KRANZINGER_P.pdf (4.25 MB)
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2016
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Kranzinger, P.P.
Kessler, M.
Krämer, E.
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http://hdl.handle.net/20.500.11881/3757
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