Accession Number:

ADA001864

Title:

Problems of Thermodynamic Equilibrium of Outflowing Combustion Products,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1974-11-12

Pagination or Media Count:

11.0

Abstract:

The goals of the present study were to measure translatory temperature, identify the radiation spectrum of a stream of combustion products from condensed systems behind the edge of the nozzle in a model engine, and establish the equilibrium condition of the system, provided it exists. The radiation spectrum of combustion products flowing from a model jet engine nozzle was studied for ballistiteH powder and a composition of H5 aluminum for two engine operating modes incomplete 20-30 at and complete 80-90 at.

Subject Categories:

  • Atomic and Molecular Physics and Spectroscopy
  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE