Progress in sub-grid scale modeling of shock-turbulence interaction

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The authors report on progress in the development of sub grid scale (SGS) closure relationships for the unresolved motion scales in compressible large eddy simulations (LES). At present they are refining the SGS model and overall LES procedure to include: a linearized viscoelastic model for finite thickness shock distortions and shocked turbulence field response; multiple scale asymptotic considerations to improve predictions of average near-wall surface behavior; and a spectral statistical model simulating the effects of high wave number stochastic feed-back from the unresolved SGS nonlinear motion influences on the explicitly resolved grid scale motions. Predicted amplification levels, modal energy partition, ... continued below

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11 p.

Creation Information

Buckingham, A.C. & Grun, J. December 1, 1994.

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  • Buckingham, A.C. Lawrence Livermore National Lab., CA (United States). Center for Advanced Fluid Dynamics Applications
  • Grun, J. Naval Research Lab., Washington, DC (United States). Plasma Physics Div.

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Description

The authors report on progress in the development of sub grid scale (SGS) closure relationships for the unresolved motion scales in compressible large eddy simulations (LES). At present they are refining the SGS model and overall LES procedure to include: a linearized viscoelastic model for finite thickness shock distortions and shocked turbulence field response; multiple scale asymptotic considerations to improve predictions of average near-wall surface behavior; and a spectral statistical model simulating the effects of high wave number stochastic feed-back from the unresolved SGS nonlinear motion influences on the explicitly resolved grid scale motions. Predicted amplification levels, modal energy partition, shock translational to turbulence kinetic energy transfer, and viscoelastic spatio-temporal response of turbulence to shock interaction are examined in comparison with available experimental evidence. Supplemental hypersonic compressible turbulence experimental information is developed from sub nanosecond interval pulsed shadowgraph evidence of laser impulse generated hypervelocity shocks interacting with intense, previously developed and carefully characterized initial turbulence. Accurate description of the influence of shock-turbulence interactions is vital for predicting their influence on: Supersonic/hypersonic flow field analysis, aerodynamic design, and aerostructural materials selection. Practical applications also include interior supersonic combustion analysis and combustion chamber design. It is also the essential foundation for accurately predicting the development and evolution of flow-field generated thermal and electromagnetic radiation important to hypersonic flight vehicle survivability, detection and communication.

Physical Description

11 p.

Notes

OSTI as DE95017859

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  • Other Information: PBD: Dec 1994

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  • Other: DE95017859
  • Report No.: UCRL-ID--119453
  • Grant Number: W-7405-ENG-48
  • DOI: 10.2172/106519 | External Link
  • Office of Scientific & Technical Information Report Number: 106519
  • Archival Resource Key: ark:/67531/metadc627992

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Creation Date

  • December 1, 1994

Added to The UNT Digital Library

  • June 16, 2015, 7:43 a.m.

Description Last Updated

  • Feb. 23, 2016, 3:25 p.m.

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Buckingham, A.C. & Grun, J. Progress in sub-grid scale modeling of shock-turbulence interaction, report, December 1, 1994; California. (digital.library.unt.edu/ark:/67531/metadc627992/: accessed December 12, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.