Accession Number:

AD0750038

Title:

Two-Phase Nozzle Flow (Gas-Solid).

Descriptive Note:

Master's thesis,

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OHIO SCHOOL OF ENGINEERING

Personal Author(s):

Report Date:

1972-06-01

Pagination or Media Count:

83.0

Abstract:

A numerical method, requiring the use of a computer, is developed to determine mass flow rates in two-phase gas-solid rocket nozzle flow. In addition to the conservation equations of total mass, momentum, and energy, a particle energy equation and equation of motion are included in the analysis. The selection of appropriate particle drag coefficients and convective heat transfer coefficients is a primary consideration in the successful utilization of the method. Author

Subject Categories:

  • Fluid Mechanics
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE