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 PDF Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324

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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 PDF Author: Charles C. Graves
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 98

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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 PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 38

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Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138

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Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 694

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Analysis of Total-pressure Loss and Airflow Distribution for Annular Gas Turbine Combustors

Analysis of Total-pressure Loss and Airflow Distribution for Annular Gas Turbine Combustors PDF Author: Robert R. Tacina
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 52

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Book Description
Computer analysis of total pressure loss and air flow distribution in annular flow gas turbine combustion chambers.

Performance of Short Length Turbojet Combustor Insensitive to Radial Distortion of Inlet Airflow

Performance of Short Length Turbojet Combustor Insensitive to Radial Distortion of Inlet Airflow PDF Author: Francis M. Humenik
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Book Description
Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow.

Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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Gas Turbine Combustion

Gas Turbine Combustion PDF Author: Arthur H. Lefebvre
Publisher: CRC Press
ISBN: 1420086057
Category : Science
Languages : en
Pages : 560

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Book Description
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