Preliminary LES Over a Hypersonic Elliptical Cross-Section Cone

Abstract

The characteristics of the hypersonic flow around an elliptical-cross section cone and the computational code to perform large-eddy simulations of this flow are described. Preliminary results of the Lagrangian implementation used to compute the subgrid-scale terms are presented.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 2001
Accession Number
ADP013702

Entities

People

  • G. V. Candler
  • G. Weirs
  • M. Pino Martı́n
  • Micah Wright
  • U. Piomelli

Organizations

  • Princeton University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Fluid Dynamics
  • Cross Flow
  • Engineering
  • Experimental Data
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Layers
  • Simulations
  • Turbulent Boundary Layer
  • Turbulent Flow
  • Universities

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow