Acoustic formulations for aeronautical and naval rotorcraft noise prediction based on the Ffows Williams and Hawkings Equation
Doctoral Thesis
(2008)
Author(s)
C Testa (TU Delft - System Engineering & Aircraft Design)
Research Group
System Engineering & Aircraft Design
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https://resolver.tudelft.nl/uuid:6b1574e3-0b3d-44df-a690-558309542d72
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Publication Year
2008
Language
English
Research Group
System Engineering & Aircraft Design
ISBN (print)
978-90-8559-358-4
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