NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Investigation of the tone-burst tube for duct lining attenuation measurementThe tone burst technique makes practical the laboratory evaluation of potential inlet and discharge duct treatments. Tone burst apparatus requires only simple machined parts and standard components. Small, simply made, lining samples are quickly and easily installed in the system. Two small electromagnetric loudspeaker drivers produce peak sound pressure level of over 166 db in the 3-square-inch sample duct. Air pump available in most laboratories can produce air flows of over plus and minus Mach 0.3 in the sample duct. The technique uses short shaped pulses of sound propagated down a progressive wave tube containing the sample duct. The peak pressure level output of the treated duct is compared with the peak pressure level output of a substituted reference duct. The difference between the levels is the attenuation or insertion loss of the treated duct. Evaluations of resonant absorber linings by the tone burst technique check attenuation values predicted by empirical formulas based on full scale ducts.
Document ID
19720015026
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Soffel, A. R.
(Advanced Technology Center, Inc. Dallas, TX, United States)
Morrow, P. F.
(Advanced Technology Center, Inc. Dallas, TX, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Subject Category
Physics, General
Report/Patent Number
NASA-CR-112031
Report Number: NASA-CR-112031
Accession Number
72N22676
Funding Number(s)
CONTRACT_GRANT: NAS1-10021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available