Inviscid Blunt Body Shock Layers (Two-Dimensional Symmetric and Axisymmetric Flows)

Abstract

The results of a time-dependent computation of blunt body shock layers for two-dimensional symmetric and axisymmetric flows are presented in a systematic form for a range of values of the free stream Mach number and bodies of different shapes and variable bluntness. A brief discussion of the relevant features of the computational technique is given. The results are presented in a graphical form; the graphs were produced by the computer.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1968
Accession Number
AD0672543

Entities

People

  • Gino Moretti

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Cyber
  • Space

DTIC Thesaurus Topics

  • Applied Mechanics
  • Axisymmetric Flow
  • Blunt Bodies
  • Bodies
  • Computational Fluid Dynamics
  • Equations
  • Flow Fields
  • Fluid Dynamics
  • Free Stream
  • Geometry
  • Mach Number
  • Mechanics
  • Military Research
  • Shock Waves
  • Stagnation Point
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.