Studies to Improve Environmental Assessments of Sonic Booms Produced during Air Combat Maneuvering

Abstract

Fighter aircraft, when engaged in air-to-air combat training maneuvers where supersonic flight is permitted, produce sonic booms. Definition of the noise environment at locations on the ground below these maneuver areas must rely on statistical descriptions of aircraft operating parameters and geographic location. This report develops distribution functions for pertinent parameters for different fighter airplanes by analysis of tracking data obtained by Air Combat Maneuvering Instrumentation at supersonic military operating areas associated with Luke and Nellis Air Force Bases. Next a variety o f pressure- time histories produced at ground microphone positions by sonic booms produced by an F-104 in a early NASA study were analyzed to obtain A-weighted and C-weighted sound levels. Particular attention was paid to the difference between peak unweighted overpressure, when expressed in decibels, and frequency-weighted sound exposure levels for sonic booms near a caustic produced by focusing during accelerated maneuvers, and as lateral cutoff conditions are approached.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1983
Accession Number
ADA138254

Entities

People

  • William J. Galloway

Organizations

  • BBN Technologies

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Computer Programs
  • Data Processing
  • Databases
  • Elevation
  • Environment
  • Fighter Aircraft
  • Mach Number
  • Measurement
  • Plastic Explosives
  • Pressure Signatures
  • Sea Level
  • Sonic Boom
  • Sound Pressure
  • Spatial Distribution
  • Two Dimensional

Readers

  • Acoustics.
  • Missile Defense Systems.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow