Published June 1982 | Version v1
Report Restricted

Flow process in combustors

Description

Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine combustors were investigated. Flow features of most interest were vorticity, especially swirl, and turbulence. Theoretical analyses, numerical calculations, and experiments were performed. The theoretical and numerical work focused on noncombusting flows, while the experimental work consisted of both reacting and nonreacting flow studies. An experimental data set, e.g., velocity, temperature and composition, was developed for a swirl flow combustor for use by combustion modelers for development and validation work

Availability note (English)

MF available from INIS under the Report Number; Available from NTIS, PC A02/MF A01.

Files

Restricted

The record is publicly accessible, but files are restricted to users with access.

Additional details

Publishing Information

Imprint Pagination
16 p.
Report number
N--8231642

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
14783725
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Numerical Data
Descriptors DEI
CHEMICAL COMPOSITION; COMBUSTION; EXPERIMENTAL DATA; GAS TURBINES; TEMPERATURE DEPENDENCE; TURBULENT FLOW; VELOCITY; VORTEX FLOW; VORTICES
Descriptors DEC
CHEMICAL REACTIONS; DATA; FLUID FLOW; INFORMATION; NUMERICAL DATA; OXIDATION; TURBINES

Optional Information

Secondary number(s)
NASA-CR--169294.