Accession Number:

AD0726118

Title:

Unsteady Combustion in Gaseous Propellant Rocket Motors

Descriptive Note:

Technical rept.

Corporate Author:

PRINCETON UNIV NJ DEPT OF AEROSPACE AND MECHANICAL SCIENCES

Personal Author(s):

Report Date:

1970-12-01

Pagination or Media Count:

395.0

Abstract:

This research work was directed toward the development of a consistent experimental and theoretical description of the phenomenon of intrinsic unstable combustion in the gas rocket. A determination was achieved of the contribution of gas phase rate processes, in particular, chemical kinetics , to the coupling of a finite-dimensional unsteady turbulent combustion zone and finite amplitude linear and nonlinear longitudinal mode pressure oscillations.

Subject Categories:

  • Combustion and Ignition
  • Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE