Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas PDF full book. Access full book title Theoretical Analysis of Total-pressure Loss and Airflow Distribution for Tubular Turbojet Combustors with Constant Annulus and Liner Cross-sectional Areas by A. J. Eggers. Download full books in PDF and EPUB format.
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
Get Book Here
Book Description
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
Get Book Here
Book Description
Author: Charles C. Graves
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 98
Get Book Here
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
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 694
Get Book Here
Book Description
Author: Robert R. Tacina
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 52
Get Book Here
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
Get Book Here
Book Description
Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow.
Author: Arthur H. Lefebvre
Publisher: CRC Press
ISBN: 1420086057
Category : Science
Languages : en
Pages : 560
Get Book Here
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
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Get Book Here
Book Description
