Preliminary review of active control technology applied to the fairing acoustic problem
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1275
Reference36 articles.
1. Eldred, K. M. "Acoustic Loads Generated by the Propulsion System,"NASA SP-8072,June 1971.
2. In-flight external and internal noise measurement for TR-I rocket nose fairing
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1. Active Structural-Acoustic Control of a Rocket Fairing Using Proof-Mass Actuators;Journal of Spacecraft and Rockets;2001-03
2. Active Acoustic Control of a Rocket Fairing Using Spatially Weighted Transducer Arrays;Journal of Spacecraft and Rockets;2001-01
3. Acoustic control of a rocket fairing using spatially weighted transducer arrays;41st Structures, Structural Dynamics, and Materials Conference and Exhibit;2000-04-03
4. Vibroacoustic modeling of a launch vehicle payload fairing for active acoustic control;39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit;1998-04-20
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