000 03157cam a2200397 i 4500
001 on1266738606
003 OCoLC
005 20240726105305.0
008 210223t20192019gw ad fob 000 0 eng d
040 _aLUN
_beng
_erda
_epn
_cLUN
_dOCLCO
_dVT2
_dS2H
_dOCLCF
_dUKKNU
_dLIP
_dUAB
_dOCLCO
_dOCLCQ
_dNT
020 _a3832549714
020 _a9783832549718
_q((electronic)l(electronic)ctronic)
050 0 4 _aTA365
_b.I584 2019
049 _aMAIN
100 1 _aBrezas, Spyros,
_e1
245 1 0 _aInvestigation on the dissemination of unit watt in airborne sound and applications /Spyros Brezas.
260 _aBerlin, Germany :
_bLogos Verlag Berlin GmbH,
_c(c)2019.
300 _a1 online resource (iv, 197 pages) :
_billustrations, charts
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _adata file
_2rda
490 1 _aAachener Beitrage zur Akustik
530 _a2
_ub
500 _aAuthor's doctoral thesis, Rheinisch-Westfälische Technische Hochschule Aachen.
504 _a1
520 0 _aSound power describes the emission of sound from sound sources. Despite today's state-of-the art measurement techniques, the current sound power determination methods are restricted due to various limitations. To overcome these limitations, a new sound power determination method is proposed, aiming at the establishment of traceability in airborne sound. This will enable the characterization of a sound source by its free field sound power. The dissertation describes a study on the dissemination process, which will allow the sound power of a device under test located at a real surrounding environment, to be referred to its free field sound power. Apart from the sound power, the corresponding uncertainty may be estimated in a transparent way, where each uncertainty component is provided. The basic tool for the dissemination process is the substitution method using aerodynamic reference sound sources, applied to both sound pressure and sound intensity measurements. Initially, a theoretical investigation deals with the factors that influence the substitution method. Experimental results are then presented based on measurements using a specially designed scanning apparatus. The transition from calibration to in situ conditions and the required correction, due to changes in environmental and operational conditions, is then discussed. In the last section, the sound power level of devices under test is determined along with its related uncertainty, which is further compared to the up-to-date uncertainty values.
650 0 _aSound
_xMeasurement.
655 1 _aElectronic Books.
700 1 _aRheinisch-Westfälische Technische Hochschule Aachen,
_edegree awarding institution.
856 4 0 _uhttps://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&db=nlabk&AN=3541175&site=eds-live&custid=s3260518
_zClick to access digital title | log in using your CIU ID number and my.ciu.edu password
936 _aBATCHLOAD
942 _cOB
_D
_eEB
_hTA
_m2019
_QOL
_R
_x
_8NFIC
_2LOC
994 _a92
_bNT
999 _c95373
_d95373
902 _a1
_bCynthia Snell
_c1
_dCynthia Snell