Theoretical Analysis Of Total Pressure Loss And Airflow Distribution For Tubular Turbojet Combustors With Constant Annulus And Liner Cross Sectional Areas
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Author | : A. J. Eggers |
Publisher | : |
Total Pages | : 324 |
Release | : 1958 |
Genre | : Aerodynamic heating |
ISBN | : |
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.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 38 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1138 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 694 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : Robert R. Tacina |
Publisher | : |
Total Pages | : 52 |
Release | : 1969 |
Genre | : Gas-turbines |
ISBN | : |
Computer analysis of total pressure loss and air flow distribution in annular flow gas turbine combustion chambers.
Author | : Francis M. Humenik |
Publisher | : |
Total Pages | : 44 |
Release | : 1970 |
Genre | : Airplanes |
ISBN | : |
Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow.
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
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 388 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |