By using the model of an aircraft fuselage discussed in Part \(\mathrm{I}\), an analysis is presented which demonstrates that the total acoustic potential energy \(\left(E_{p}\right)\) within the cylindrical model is minimized by a unique vector of secondary force inputs. Similar analysis is used to
Active control of sound inside a sphere via control of the acoustic pressure at the boundary surface
โ Scribed by N. Epain; E. Friot
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 504 KB
- Volume
- 299
- Category
- Article
- ISSN
- 0022-460X
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