Current research has focused on the reduction of sound transmission through the aircraft fuselage into the interior of aircraft due to turbulent boundary layer excitation. The present work utilizes an analytical model, previously developed by the authors, as a design tool in the development of feedb
Control strategies and mechanisms for active control of sound transmission into a vibro-acoustic enclosure
โ Scribed by Guoyong Jin; Na Feng; Tiejun Yang
- Book ID
- 107512950
- Publisher
- Harbin Engineering University
- Year
- 2011
- Tongue
- English
- Weight
- 525 KB
- Volume
- 10
- Category
- Article
- ISSN
- 1671-9433
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