Helicopter Aural Detectability

Abstract

The principal objective of the study is to develop the methodology for the prediction of helicopter aural detection thresholds from measured or estimated parameters of significance. The subjective aspects of helicopter noise are discussed. A review is presented of the effects of atmospheric and terrain features upon the observed sound, and of the limitations in the measurement and analysis of helicopter noise. An experimental program is described, in which a group of subjects listened to a large number of synthetic and recorded helicopter sounds inside a specially designed acoustic chamber. Through these experiments, a model for calculating aural detection thresholds is developed, tested, and found to be accurate to within plus or minus 4dB. Appendices to the report include detailed instructions for applying several versions of the developed method and also provide simplified procedures for estimating propagation losses.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1971
Accession Number
AD0730788

Entities

People

  • John B. Ollerhead

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Acoustics
  • Aircrafts
  • Analyzers
  • Atmospheric Attenuation
  • Bandwidth
  • Boundary Layer
  • Data Acquisition
  • Data Analysis
  • Detection
  • Diffraction
  • Doppler Effect
  • Ear
  • Frequency Bands
  • Measurement
  • Medical Personnel
  • Recording Systems
  • Turbines

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Computer Vision.
  • Systems Analysis and Design