Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas

Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas
Author: Charles C. Graves
Publisher:
Total Pages: 98
Release: 1958
Genre: Aeronautics
ISBN:

The combustor total-pressure-loss coefficient and liner air-flow distribution are presented graphically in terms of the following dimensionless parameters: (1) combustor reference Mach number, (2) ratio of combustor-exit to inlet total temperature, (3) fraction of total airflow passing through the liner dome, (4) ratio of total open hole area in liner wall to total combustor cross-sectional area, and (5) ratio of liner cross-sectional area to total combustor cross-sectional area.

Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 38
Release: 1958
Genre: Aeronautics
ISBN:

Report

Report
Author:
Publisher:
Total Pages: 1138
Release: 1958
Genre: Aeronautics
ISBN:

Gas Turbine Combustion

Gas Turbine Combustion
Author: Arthur H. Lefebvre
Publisher: CRC Press
Total Pages: 560
Release: 2010-04-26
Genre: Science
ISBN: 1420086057

Reflecting the developments in gas turbine combustion technology that have occurred in the last decade, Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition provides an up-to-date design manual and research reference on the design, manufacture, and operation of gas turbine combustors in applications ranging from aeronautical to po