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A New Simulator for Assessing Subjective Effects of Sonic BoomsA man rated and computer driven sonic boom simulator which has been constructed and placed in operational use at NASA-Langley is described. The simulator is used to study human subjective reactions to sonic booms and has the capability of producing a wide range of signatures under controlled conditions. Results are presented to illustrate the capability of the simulator to generate user specified N-wave and shaped booms having rise times as low as 0.5 milliseconds and peak overpressures up to 191 Pa (4 psf). The validity of the simulator as a lab research tool for studying human subjective response to sonic booms was demonstrated by successful completion of a preliminary test designed to compare loudness of N-wave sonic booms with results obtained by other investigators. Excellent agreement of the preliminary test data with existing data was observed. This provided confidence in the experimental methodology and established the simulator as a viable tool for performing detailed evaluations of sonic boom loudness and acceptability within the lab. environment.
Document ID
19920002541
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Leatherwood, Jack D.
(NASA Langley Research Center Hampton, VA, United States)
Shepherd, Kevin P.
(NASA Langley Research Center Hampton, VA, United States)
Sullivan, Brenda M.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Acoustics
Report/Patent Number
NASA-TM-104150
NAS 1.15:104150
Accession Number
92N11759
Funding Number(s)
PROJECT: RTOP 537-03-21-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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