Floating Shock Fitting Via Lagrangian Adaptive Meshes.

Abstract

In recent works we have formulated a new approach to compressible flow simulation, combining the advantages of shock-fitting and shock-capturing. Using a cell-centered Roe scheme discretization on unstructured meshes, we warp the mesh while marching to steady state, so that mesh edges align with shocks and other discontinuities. This new algorithm, the Shock-fitting Lagrangian Adaptive Method (SLAM) is, in effect, a reliable shock-capturing algorithm which yields shock-fitted accuracy at convergence. Shock-capturing algorithms like this, which warp the mesh to yield shock-fitted accuracy, are new and relatively untried. However, their potential is clear. In the context of sonic booms, accurate calculation of near-field sonic boom signatures is critical to the design of the High Speed Civil Transport (HSCT). SLAM should allow computation of accurate N-wave pressure signatures on comparatively coarse meshes, significantly enhancing our ability to design low-boom configurations for high-speed aircraft. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1994
Accession Number
ADA289758

Entities

People

  • John Van Rosendale

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Algorithms
  • Bow Shock
  • Compressible Flow
  • Computations
  • Discontinuities
  • Flow Fields
  • Near Field
  • Path Integrals
  • Pressure Signatures
  • Shock Waves
  • Sonic Boom
  • Steady State
  • Supersonic Aircraft
  • Three Dimensional
  • Waves

Fields of Study

  • Physics

Readers

  • Brain and Cognitive Science; Experimental Psychology; Cognitive Neuroscience
  • Computational Fluid Dynamics (CFD)
  • Computer Vision.