NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Status of cavity noise phenomena measurement and suppression on the B-1 aircraftDuring the B-1 aircraft development, an extensive program of weapons bay cavity noise measurement and suppression studies was performed using wind tunnel models, flight test measurements, and aircraft design modifications. Substantial cavity noise reduction was demonstrated during flight test operations. The unsuppressed cavity noise level of 170 dB was reduced to values less than 150 dB with external retractable spoilers upstream of the cavity opening.
Document ID
19800007942
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tipton, A. G.
(Rockwell International Corp. El Segundo, CA, United States)
Hodson, C. H.
(Rockwell International Corp. El Segundo, CA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: Shock and Vibration Inform. Center The Shock and Vibration Bull., Pt 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
80N16202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available