Effects of Diffuser Inlet Velocity Profile on Gas Turbine Combustor Performance
Author : Richard Adkins
Publisher :
Page : pages
File Size : 37,26 MB
Release : 1977
Category :
ISBN :
Effects of Radial and Circumferential Inlet Velocity Profile Distortions on Performance of a Short-length Double-annular Ram-induction Combustor
Author : Donald F. Schultz
Publisher :
Page : 52 pages
File Size : 23,47 MB
Release : 1972
Category : Aircraft gas-turbines
ISBN :
Book Description
Inlet air velocity profile tests were conducted on a full-scale short-length 102-centimeter-diameter annual combustor designed for advanced gas turbine engine applications. The inlet profiles studied include radial distortions that were center peaked, and tip peaked, as well as a circumferential distortion which was center peaked for one-third of the circumference and flat for the other two-thirds. An increase in combustor pressure loss was the most significant effect of the radial air velocity distortions. With the circumferential distortion, exit temperature pattern factor doubled when compared to a flat velocity profile.
GAS Turbine Combustion, Second Edition
Author : Arthur H. Lefebvre
Publisher : CRC Press
Page : 420 pages
File Size : 45,58 MB
Release : 1998-09-01
Category : Technology & Engineering
ISBN : 9781560326731
Book Description
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.
Effect of Diffuser Bleed on Performance of an Annular Swirl Can Combustor
Author : Albert J. Juhasz
Publisher :
Page : 30 pages
File Size : 13,22 MB
Release : 1974
Category : Aircraft gas-turbines
ISBN :
Book Description
Gas Turbine Combustion
Author : Arthur H. Lefebvre
Publisher : CRC Press
Page : 560 pages
File Size : 12,26 MB
Release : 2010-04-26
Category : Science
ISBN : 1420086057
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
Effect of Various Diffuser Designs on the Performance of an Experimental Turbojet Combustor Insensitive to Radial Distortion of Inlet Airflow
Author : James A. Biaglow
Publisher :
Page : 28 pages
File Size : 15,17 MB
Release : 1971
Category :
ISBN :
Book Description
The Effect of an Exhaust Diffuser on the Performance of a Gas Turbine
Author : Chester Joseph Blechinger
Publisher :
Page : 238 pages
File Size : 32,72 MB
Release : 1966
Category : Diffusers
ISBN :
Book Description
Performance of a Vortex-controlled Diffuser in an Annular Swirl-can Combustor at Inlet Mach Numbers Up to 0.53
Author : John Milton Smith
Publisher :
Page : 24 pages
File Size : 33,9 MB
Release : 1979
Category : Diffusers
ISBN :
Book Description
Effect of Wall Edge Suction on the Performance of a Short Annular Dump Diffuser with Exit Passage Flow Resistance
Author : Albert J. Juhasz
Publisher :
Page : 38 pages
File Size : 14,54 MB
Release : 1975
Category : Aircraft gas-turbines
ISBN :
Book Description
NASA Technical Note
Author :
Publisher :
Page : 542 pages
File Size : 48,21 MB
Release : 1974
Category : Aeronautics
ISBN :
