This is the Structural Acoustics Branch website. The Structural Acoustics Branch is part of the Aerodynamics, Aerothermodynamics. and Acoustics Competency at the National Aeronautics and Space Administration's Langley Research CenterUse this link to skip repetitive navigation links and information.

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NASA Official
Responsible for Site:
Dr. Kevin P. Shepherd

Page Curator:
David A. McCurdy

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Last Updated
March 6, 2007

The Acoustics Research Laboratory for aircraft noise research ...

The Acoustics Research Laboratory (ARL) provides the principal focus for acoustics research at Langley Research Center. The building houses the offices of the Structural Acoustics Branch and several of the major acoustic research facilities.. The primary research facilities include a 20 ft. x 24 ft. x 30 ft. anechoic quiet-flow facility with two open-jet wind tunnels, a 21 ft. x 31 ft. x 15 ft. reverberation chamber, a two-chamber aircraft sidewall noise transmission measurement facility, and the human-response-to-noise laboratories. The ARL is used to conduct acoustic studies of aircraft components and models and to conduct subjective acoustic studies that involve actual test subjects.

For more information about some of the acoustics facilities used by the Structual Acoustics Branch, follow the links below.

Aircraft Interior Acoustic Simulator

Flow Impedance Test Facility

Thermal Acoustic Fatigue Apparatus

Structural Acoustics Loads and Transmission Facility