Hypervelocity Flow over Spheres. Appendix B.

Abstract

The following important results were obtained from investigations of chemically reacting blunt body flows and of shock wave interactions in hypervelocity flow: (1) A new view of the binary scaling concept resulted from experimental and theoretical work on flow over spheres, in terms of two dimensionless parameters. (2) The evolution of the vorticity generated by a curved shock wave could be visualized with resonant enhancement of streak lines. (3) The effect of recombination in flow along a streamline after a curved shock was explained. (4) Previous predictions of greatly enhanced heat flux by real gas effects in shock on shock interactions were not borne out. (5) The study provided extensive corroboration of the computed free stream conditions in the free piston shock tunnel T5. (6) A number of improvements of shock tunnel technology were made. especially regarding diaphragm manufacture, nozzle throat material, and computation of the processes during operation. (7) Improved diagnostic techniques were generated. including low noise coaxial thermocouple gauges and inexpensive high quality holographic interferometry.

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Document Details

Document Type
Technical Report
Publication Date
Feb 02, 1996
Accession Number
ADA306378

Entities

People

  • Chihyung Wen

Organizations

  • California Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chemical Reactions
  • Chemistry
  • Computational Fluid Dynamics
  • Computational Science
  • Dye Lasers
  • Energy Transfer
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Hydrodynamics
  • Jet Propulsion
  • Liquid Dye Lasers
  • Physics Laboratories
  • Shock Tunnels
  • Vibrational Relaxation

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow