Community Noise Exposure Resulting from Aircraft Operations. Volume 4. Acoustic Data on Air Force Trainer/Fighter Aircraft,

Abstract

This report presents the results of field test measurements to define the noise produced on the ground by military, fixed wing aircraft during controlled level flyovers and ground runups. For flight conditions, data are presented in terms of various acoustic measures over the range 200-25,000 feet minimum slant distance to the aircraft. For ground runups, data are presented as a function of angle and distance to the aircraft. All of the data are normalized to standard acoustic reference conditions of 59 deg. F temperature and 70% relative humidity. Noise data are presented in this Volume 4 for the following aircraft: F-100C, D, F; F-101B, C, F; F-102A; F-105B, D, F, G; F-106A, B; T-33A; T-37B; T-38A; T-39A, B, F; T-43A; and U-2.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1978
Accession Number
ADA053702

Entities

People

  • Jerry D. Speakman
  • Robert A. Lee
  • Robert G. Powell

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Biomedical

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Aircraft Noise
  • Aircrafts
  • Biomedical Research
  • Celestial Navigation
  • Environment
  • Field Tests
  • Fighter Aircraft
  • Fixed Wing Aircraft
  • Operating Systems
  • Plastic Explosives
  • Security
  • Self Assembly
  • Test Methods
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Aerospace Engineering
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