AN EXPERIMENTAL STUDY OF SOME BASE INJECTION TECHNIQUES AND THE EFFECT OF LARGE PRESSURE GRADIENTS ON TURBULENT DIFFUSION PROCESSES.

Abstract

Results of an experimental study of some base injection techniques and the effect of large pressure gradients on turbulent diffusion processes in an axisymmetric flow past a slender body at Mach number 3.92 and Reynolds number 3.85 x 10 to the 7th power ft. are presented. Base injection techniques were studied using gaseous hydrogen, helium, nitrogen, and argon as injectants. In each case, it is noticed that the base pressure reaches its peak value much faster (i.e., for a smaller injection rate) with a low molecular weight gas and that a larger increase in base pressure is accomplished with the lighter gas. Some schemes show very irregular behavior in the variation of base pressure with injection. In the study of diffusion processes it is found that the mass diffusion process is not affected at all by the pressure gradients produced in the flow field and that mass, momentum, and thermal diffusion are not the same. This leads to the conclusion that assumptions of Lewis number, Prandtl number, and Schmidt number equal to unity are not correct, especially for problems with large pressure gradients. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1968
Accession Number
AD0679218

Entities

People

  • Herbert Fox
  • Ram Sinha
  • Victor Zakkay

Organizations

  • New York University

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Axisymmetric Flow
  • Base Pressure
  • Diffusion
  • Flow
  • Flow Fields
  • Mach Number
  • Molecular Weight
  • Peak Values
  • Prandtl Number
  • Pressure Gradients
  • Reynolds Number
  • Slender Bodies
  • Thermal Diffusion
  • Turbulent Diffusion

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.