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AIR1672
Practical Methods to Obtain Free-Field Sound Pressure Levels from Acoustical Measurements Over Ground Surfaces
Practical Methods to Obtain Free-Field Sound Pressure Levels from Acoustical Measurements Over Ground Surfaces
2012-07-01
有效
【范围】 2. INTRODUCTION: Acqui sition of free-field data is of practical significance in the field of aeronautical acoustics. The need for free-field data includes (but is not restricted to) the following: (1) comparison of acoustical data obtained from the same engi ne under various measurement conditions, (2) com- pari son of the results obtained from node!s with those from an engine on a test stand, (3) comparison of noise measurements made on the same engine under static and in-flight conditions, (4) design of test facilities, (5) standardization of techniques for "in situ" acoustical measurements, (6) spectral decomposition to isolate the contribution of different sources to the total noise, and (7) prediction of aircraft noi se on the basis of methods which, generally, provide free-field data. There is an increasing tendency to test full-scale engi ne components and scale models in anechoic test facilities that provide free-field conditions. This AIR complements this work by identifying those methods in current use which provide free-field acoustic data for measurements on engines under static conditions in the presence of a ground surface. Separate Appendices to thi s AIR describe different methods for noi se measurement in the field that conform with the state-of-the-art to a certain extent. That is, each method has generally been systematical ly used hy at least one organization and has been substantiated by data obtained from at least one test site. Si nee the international ly standardized methods of obtaining flight test noise levels suffer from the same ground reflection interference effects as measurements above the ground plane in the vicinity of a test stand, one appendix describes alternative measurement procedures for the overflight case, together with simplified adjustments to obtain approximate free-field sound pressure level s. Each Appendix is dated, is subject to later modifications when additional data become available, and provides an approach to a particular technique presented by a member of the A-21 Committee. The following section discusses certain practical aspects of ground reflection effects.strRefField
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PROBABILITY DISTRIBU
EMPIRICAL REFLECTION
ILLUSTRATION OF EFF
COMPARISON OF SPECTR
EXAMPLE OF APPLICATI
EXAMPLE OF SPECTRUM
BOEING ENGINE TEST S
FIGURE B2. BOEING EN
FIGURE B3. SCHEMATIC
MICROPHONE LOCATIONS
G R O U N D A N D P
EFFECT OF E L E V A
Cl P ratt & W h i t
C2 G e o m e t r y o
C3 T y p i c a l Jet
C 4 Spec t r a M e a
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C 5 Axial Jet N o i
C 6 S p e c t r a M
formula 9
C7 Specific N o r m
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formula 11
formula 12
formula 14
C 8 C o m p a r i s
Dl
D 2
D3
D3 (C o nt . )
D4
D 5
D6
D 7
D7 (Cont.)
D8
D9
D10
D 11
D12

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