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  • 1
    Publication Date: 2019-06-27
    Description: A study plan for quantifying the relationship between human annoyance and the noise level of individual aircraft events is studied. The validity of various noise descriptors or noise metrics for quantifying aircraft noise levels are assessed.
    Keywords: ENVIRONMENT POLLUTION
    Type: NASA-TM-81803
    Format: application/pdf
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  • 2
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    In:  CASI
    Publication Date: 2019-07-13
    Description: A computer model was developed to assess the noise impact of an airport on the community which it serves. Assessments are made using the Fractional Impact Method by which a single number describes the community aircraft noise environment in terms of exposed population and multiple event noise level. The model is comprised of three elements: a conventional noise footprint model, a site specific population distribution model, and a dose response transfer function. The footprint model provides the noise distribution for a given aircraft operating scenario. This is combined with the site specific population distribution obtained from a national census data base to yield the number of residents exposed to a given level of noise. The dose response relationship relates noise exposure levels to the percentage of individuals highly annoyed by those levels.
    Keywords: ENVIRONMENT POLLUTION
    Type: NASA-TM-80198 , Acoust. Soc. of Am. Meeting; Nov 26, 1979 - Nov 30, 1979; Salt Lake City, UT; United States
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: The Fraction Impact Method (FIM), developed by the National Research Council (NRC) for assessing the amount and physiological effect of noise, is described. Here, the number of people exposed to a given level of noise is multiplied by a weighting factor that depends on noise level. It is pointed out that the Aircraft-noise Levels and Annoyance MOdel (ALAMO), recently developed at NASA Langley Research Center, can perform the NRC fractional impact calculations for given modes of operation at any U.S. airport. The sensitivity of these calculations to errors in estimates of population, noise level, and human subjective response is discussed. It is found that a change in source noise causes a substantially smaller change in contour area than would be predicted simply on the basis of inverse square law considerations. Another finding is that the impact calculations are generally less sensitive to source noise errors than to systematic errors in population or subjective response.
    Keywords: ENVIRONMENT POLLUTION
    Type: In: Noise-Con 81; Jun 08, 1981 - Jun 10, 1981; Raleigh, NC
    Format: text
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