Numerical Simulation of Transient Hypervelocity Flow in an Expansion Tube

Abstract

Several numerical simulations of the transient flow of helium in an expansion tube are presented in an effort to identify some of the basic mechanisms which cause the noisy test flows seen in experiments. The calculations were performed with an axisymmetric Navier-Stokes code based on a finite-volume formulation and upwinding techniques. Although laminar flow and ideal bursting of the diaphragms was assumed, the simulations showed some of the important features seen in the experiments. In particular, the discontinuity in tube diameter at the primary diaphragm station introduced a transverse perturbation to the expanding driver gas and this perturbation was seen to propagate into the test gas under some flow conditions. The disturbances seen in the test flow can be characterized as either small-amplitude, low-frequency noise possibly introduced during shock compression or large-amplitude, high- frequency noise associated with the passage of the reflected head of the unsteady expansion.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1992
Accession Number
ADA249232

Entities

People

  • P. A. Jacobs

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Transition
  • Computational Fluid Dynamics
  • Computational Science
  • Computers
  • Engineering
  • Equations
  • Flow
  • Frequency
  • Frequency Shift
  • High Pressure
  • Hypervelocity Flow
  • Layers
  • Measurement
  • Pressure Distribution
  • Simulations
  • Specific Heat

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

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