Interim Research Performance Report (Contract N00014-11-1-0752, The University of Mississippi)

Abstract

Goal: Enhance the understanding of the effect that near-nozzle and inner-nozzle flow conditions have on jet noise radiation; Objective 1- High-fidelity characterization of a heated, over-expanded supersonic jet; Objective 2- Source identification through development of advanced analytical diagnostics; Objective 3- Enhanced computational modeling of hot supersonic jets.

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Document Details

Document Type
Technical Report
Publication Date
Jun 18, 2013
Accession Number
ADA587645

Entities

People

  • Brian S Thurow
  • Charles E. Tinnet
  • Nathan E. Murray
  • Praveen Panickar

Organizations

  • University of Mississippi

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Acoustics
  • Acquisition
  • Algorithms
  • Boundary Layer
  • Computational Fluid Dynamics
  • Data Acquisition
  • Data Analysis
  • Data Sets
  • Detection
  • Frequency
  • Image Processing
  • Large Eddy Simulation
  • Phased Arrays
  • Pressure Distribution
  • Simulations
  • Three Dimensional
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Military Science and Technology Research and Modernization.
  • Software Engineering

Technology Areas

  • Hypersonics