In this article the elements of the synthesis procedure of automatic reduction system vibro-acoustic radiation, which is based on active methods by applying the original vibroacoustic field compensating effects. It is concluded that the structural stability of the synthesized system must be controlled in terms of vibration.
Keywords:
methods to reduce noise, vibroacoustic field, aircraft noise
Reference:
Tsytrytska,
L.M.
(2014),
"Osoblyvosti strukturnoho syntezu systemy znyzhennia vibroakustychnoho navantazhennia na operatoriv skladnykh system" ,
Science and Technology of the Air Force of Ukraine,
No.
3(16),
pp. 45-48.
УКР
