Acoustic formulations for aeronautical and naval rotorcraft noise prediction based on the Ffows Williams and Hawkings Equation

Doctoral thesis (2008)

Authors

C Testa System Engineering & Aircraft Design
Research Group
System Engineering & Aircraft Design
More Info
expand_more

Published Date

2008

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Research Group

System Engineering & Aircraft Design