Double‐Wall Noise Control Enclosure for an Impulsive Sound Source

Noise Control ◽  
1961 ◽  
Vol 7 (5) ◽  
pp. 12-17
Author(s):  
R. M. Hoover ◽  
L. J. Williams ◽  
W. G. Russert
1961 ◽  
Vol 33 (6) ◽  
pp. 834-834
Author(s):  
Robert M. Hoover ◽  
Lloyd J. Williams

AIHAJ ◽  
1961 ◽  
Vol 22 (6) ◽  
pp. 448-454
Author(s):  
R. M. Hoover ◽  
L. J. Williams ◽  
W. G. Russert

1997 ◽  
Vol 34 (6) ◽  
pp. 802-810 ◽  
Author(s):  
Yen Wei ◽  
Rimas Vaicaitis

電腦學刊 ◽  
2021 ◽  
Vol 32 (6) ◽  
pp. 248-253
Author(s):  
Chaofeng Lan Chaofeng Lan ◽  
Lei Zhang Chaofeng Lan ◽  
Shou Lv Lei Zhang ◽  
Rongrong Han Shou Lv


2013 ◽  
Vol 333-335 ◽  
pp. 2142-2145
Author(s):  
Qing Fu Kong ◽  
Yu Liang Dai ◽  
Shi Jian Zhu ◽  
Jia Ming Wu

In order to find a solution to the control of low frequency noise in the cabin of turboprop driven aircraft, an experimental active noise control (ANC) system is introduced in the paper, which consists of vibroacoustic field analogue subsystem, acoustic field measurement subsystem and acoustic barrier exciter subsystem. Effects of both different spaces between the primary sound source and secondary sound source of the ANC system and different frequency noises on noise-reduction result are investigated based on the experimental platform. Results of the experiment show a significant potential of the ANC method for the control of low frequency noise in the cabin of turboprop driven aircraft.


2009 ◽  
Vol 2009 (0) ◽  
pp. _357-1_-_357-6_
Author(s):  
Toshihiko KOMATSUZAKI ◽  
Yoshio IWATA ◽  
Junya KURODA

Sign in / Sign up

Export Citation Format

Share Document