Aerodynamic Noise Simulation in Sonic Fatigue Facility

Abstract

The possibility of simulating a turbulent boundary-layer noise environment using the air-flow capability of the RTD Sonic Fatigue Facility is investigated. The philosophy is adopted that it is the mechanical power absorbed by the structure from the environment that is to be duplicated. Calculations are developed that allow the prediction of the mechanical power injected into a structure by a turbulent boundary layer (TBL), and by a turbulent wall-jet. The possibility of replacing the power injected by the TBL by using turbulent wall-jets impinging on a structural model of a section of a supersonic transport is studied. Results indicate that high-frequency excitation (above 1kHz) can be adequately simulated, but that the air-flow capabilities of the facility would be exceeded by an attempt to excite a structure as large as the one chosen by a set of wall-jets at lower frequencies.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0648022

Entities

People

  • Colin G. Gordon
  • Francis M. Wiener
  • Raya Stern
  • Richard H. Lyon

Organizations

  • BBN Technologies

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • Computational Fluid Dynamics
  • Convection
  • Department Of Defense
  • Engineers
  • Fluid Dynamics
  • Frequency Bands
  • Governments
  • Jet Propulsion
  • Mach Number
  • Measurement
  • Standards
  • Supersonic Transport Aircraft
  • Test Facilities
  • United States Government

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics