AN ANALYTICAL APPROACH TO THE TURBULENT MIXING OF COAXIAL JETS,

Abstract

The turbulent mixing of coaxial jets is a critical phenomenon in areas such as air-augmented rocket propulsion and radar attenuation by rocket exhausts. In the report a model is developed which approximates the mixing of coaxial jets assuming equal pressures in the two flows. Provision is made for chemical reaction and heat release in the mixing region. The model is based on the theory developed by Libby and assumes that turbulent mixing can be described by the equations for laminar flow, if the laminar transport coefficients are replaced by their turbulent counterparts. The model is demonstrated for an afterburning rocket exhaust, and contours of velocity and temperature in the plume are constructed. Accurate predictions of microwave attenuation and infrared emission by rocket plumes were made on the basis of this model and appropriate thermochemical calculations. A simple computer solution is given. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1966
Accession Number
AD0646319

Entities

People

  • Andrew C. Victor
  • Roger W. Buecher

Organizations

  • Naval Air Weapons Station China Lake

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Afterburning
  • Attenuation
  • Chemical Reactions
  • Coefficients
  • Combustion
  • Computers
  • Emission
  • Equations
  • Flow
  • Laminar Flow
  • Microwaves
  • Mixing
  • Rocket Exhaust
  • Rocket Propulsion
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Rocket Propulsion.