Accession Number:

ADA053791

Title:

Combustor Design and Operation for a Sub-Scale Turbojet Test Cell.

Descriptive Note:

Master's thesis,

Corporate Author:

NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s):

Report Date:

1978-03-01

Pagination or Media Count:

44.0

Abstract:

A high pressure, water-cooled ramjet-type combustor capable of producing various amounts of particulates has been designed, constructed and operated in the sub-scale turbojet test cell. The combustor can be utilized to perform further studies concerning the effects of engine operating characteristics and test cell design on particulate concentrations, and also the effects of fuel additives on the amount and composition of particulates emitted. Author

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE