NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An impulse test technique with application to acoustic measurementsA method has been presented for measuring the acoustic properties of an absorbent material and a duct/nozzle system (with or without airflow) using a high voltage spark discharge as an impulse source of sound. The cross-spectra of the incident, reflected and transmitted acoustic pressure transients are analyzed by way of a FFT digital processor in the form of complex transfer functions. These transfer functions have a direct relationship to the termination impedance and radiation directivity. The impulse method has been justified by comparisons, with data obtained from existing methods (both experimental and theoretical), that show excellent agreement. Reflection coefficients and radiation impedances of various duct-nozzle systems and their associated far-field directivities are also presented as some of the applications of the impulse technique.
Document ID
19790042877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salikuddin, M.
(Lockheed-Georgia Co. Marietta, GA, United States)
Dean, P. D.
(Lockheed-Georgia Co. Marietta, GA, United States)
Plumblee, H. E., Jr.
(Lockheed-Georgia Co. Marietta, GA, United States)
Ahuja, K. K.
(Lockheed-Georgia Co. Marietta, Ga., United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 79-0679
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aeroacoustics Conference
Location: Seattle, WA
Start Date: March 12, 1979
End Date: March 14, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A26890
Funding Number(s)
CONTRACT_GRANT: NAS3-20797
Distribution Limits
Public
Copyright
Other

Available Downloads

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