Combustor design and operation for a subscale turbojet test cell
Authors
Charest, Jerry Russell
Subjects
Turbojet test cell
engine simulation
engine simulation
Advisors
Netzer, D.W.
Date of Issue
1978-03
Date
Publisher
Language
en_US
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.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.