Human Response to Sound: The Calculation of Perceived Level, PLdB (Noisiness or Loudness) Directly from Physical Measures.

Abstract

The relationship between the perceived level, PLdB, of sound (loudness or noisiness) is shown to be a function of the sound pressure squared and the sound frequency squared. A logarithmic formula employing this basic relationship between perceived level and pressure and frequency has been developed and is found to be as accurate as the more complex methods currently in use. The results are found to be more accurate than the complex methods currently in use for the useful range of sound pressure levels and frequencies found to be associated with operational aircraft including helicopters, turbofan, turboprop and turbojet powered aircraft. This work, therefore, provides the systems engineer an easily understood and useful design and evaluation method. The formula developed clearly shows the design engineer and management personnel the relationship between the physical characteristics of an evolving system and its potential impact on human and community response.

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Document Details

Document Type
Technical Report
Publication Date
Nov 17, 1976
Accession Number
ADA035677

Entities

People

  • Thomas H. Higgins

Organizations

  • Federal Aviation Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Engineers
  • Frequency
  • Helicopters
  • Jet Aircraft
  • Loudness
  • Management Personnel
  • Personnel Management
  • Sound Pressure
  • Systems Engineering
  • Turbofan Engines
  • Turbojet Engines
  • Turboprop Engines

Readers

  • Acoustics.
  • Approximation Theory.
  • Software Engineering.