Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas PDF Download
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Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
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Book Description
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
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Book Description
Author: Charles C. Graves
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 98
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Book Description
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.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 38
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 694
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Book Description
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.
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.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Book Description
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
