Broadband active structural acoustic control of aircraft cabin noise - Laboratory tests

3rd AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1997, Pages 422-431

  Mathur, G P ^a   Tran, B N ^a   Simpson, M A ^a   Peterson, D K ^b  

^a BOEING COMPANY   (United States)

^b SRI INTERNATIONAL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACTIVE NOISE CONTROL; ACTUATORS; AEROACOUSTICS; AIRCRAFT CONTROL; ARCHITECTURAL ACOUSTICS; CABINS (AIRCRAFT); FINITE ELEMENT METHOD; LOCATION; MICROPHONES; NOISE ABATEMENT; PIEZOELECTRIC ACTUATORS; TRANSFER FUNCTIONS;

ACTIVE NOISE CONTROL (ANC); ACTIVE STRUCTURAL ACOUSTIC CONTROL; AIRCRAFT APPLICATIONS; AIRCRAFT CABIN NOISE; DEMONSTRATION TESTS; DESIGN AND DEVELOPMENT; MICROPHONE SENSORS; RESEARCH FACILITIES;

FUSELAGES;

EID: 84977107102     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1997-1636     Document Type: Conference Paper

References (3)

1. Simpson, M. A. et al, “Full Scale Demonstration Tests of Cabin Noise Reduction Using Active Control,” Proc. Inter-Noise 89, pp. 459-462 (1989).
2. Elliot, S. J. et al, “In-Flight Experiments on the Active Control of Propeller-Induced Cabin Noise,” Journal of Sound and Vibration, Vol 140(2), pp. 219-238 (1990).
3. Fink, R. et al, “MD-80 Active Noise Control Flight Demonstration,” AIAA Paper 93-4439 (1993).