NASA Technical Paper
Author :
Publisher :
Page : 430 pages
File Size : 32,81 MB
Release : 1983
Category : Astronautics
ISBN :
Author :
Publisher :
Page : 430 pages
File Size : 32,81 MB
Release : 1983
Category : Astronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 634 pages
File Size : 12,24 MB
Release : 1977
Category : Aeronautics
ISBN :
Author : Arthur H. Lefebvre
Publisher : CRC Press
Page : 420 pages
File Size : 34,69 MB
Release : 1998-09-01
Category : Technology & Engineering
ISBN : 9781560326731
This revised edition provides understanding of the basic physical, chemical, and aerodynamic processes associated with gas turbine combustion and their relevance and application to combustor performance and design. It also introduces the many new concepts for ultra-low emissions combustors, and new advances in fuel preparation and liner wall-cooling techniques for their success. It details advanced and practical approaches to combustor design for the clean burning of alternative liquid fuels derived from oil shades, tar sands, and coal. Additional topics include diffusers, combustion performance fuel injection, combustion noise, heat transfer, and emissions.
Author : Arthur H. Lefebvre
Publisher : CRC Press
Page : 560 pages
File Size : 32,80 MB
Release : 2010-04-26
Category : 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 : Charles C. Graves
Publisher :
Page : 98 pages
File Size : 19,67 MB
Release : 1958
Category : 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 :
Publisher :
Page : 542 pages
File Size : 43,99 MB
Release : 1974
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 574 pages
File Size : 33,29 MB
Release : 1971
Category :
ISBN :
Author : Panel on Propulsion Effluents
Publisher :
Page : 498 pages
File Size : 42,28 MB
Release : 1975
Category : Air
ISBN :
Author : Allen J. Metzler
Publisher :
Page : 34 pages
File Size : 30,20 MB
Release : 1956
Category : Airplanes
ISBN :
Author : Jack Grobman
Publisher :
Page : 90 pages
File Size : 14,84 MB
Release : 1974
Category : Air
ISBN :