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:

Published: 1958

Total Pages: 98

ISBN-13:

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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:

Published: 1958

Total Pages: 38

ISBN-13:

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Gas Turbine Combustion
Gas Turbine Combustion

Author: Arthur H. Lefebvre

Publisher: CRC Press

Published: 2010-04-26

Total Pages: 560

ISBN-13: 1420086057

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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