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Author : Richard J. McCafferty
Publisher : Unknown
Page : 32 pages
File Size : 50,9 Mb
Release : 1950
Category : Aeronautics
ISBN : UOM:39015086432161
Author : Nicholas R. Marchionna,Arthur M. Trout
Publisher : Unknown
Page : 44 pages
File Size : 44,8 Mb
Release : 1970
Category : Airplanes
ISBN : UIUC:30112106877274
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 382 pages
File Size : 43,9 Mb
Release : 1959
Category : Aeronautics
ISBN : IND:30000092352917
Author : Anonim
Publisher : Unknown
Page : 388 pages
File Size : 46,5 Mb
Release : 1957
Category : Aeronautics
ISBN : UVA:X004173287
Author : Anonim
Publisher : Unknown
Page : 710 pages
File Size : 46,8 Mb
Release : 1973
Category : Aeronautics
ISBN : UOM:39015006098415
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 716 pages
File Size : 41,6 Mb
Release : 1956
Category : Aeronautics
ISBN : OSU:32435062280276
Author : A. M. Mellor
Publisher : Unknown
Page : 578 pages
File Size : 40,7 Mb
Release : 1990
Category : Technology & Engineering
ISBN : UOM:39015018925852
Lower pollutant emissions and broader multifuel flexibility are driving forces for advancing aircraft, vehicular, and industrial engine performance and versatility. Both are inherently connected with the design of the fuel injector and combustor system. The traditional concerns, improving durability and fuel economy over the life of the engine, remain additional requirements.**This volume offers a comprehensive treatment of modern practice aimed both at those in the field and newcomers interested in research and development for gas turbine combustors. Detailed description and assessment of a range of combustor design models and methods**Specification and evolution of fuels and fuel injectors**System models for fuel effects on engines and airframes**Evaluation of laser-based measurement techniques for combustor flow field studies
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 600 pages
File Size : 44,7 Mb
Release : 1952
Category : Aeronautics
ISBN : PSU:000009849709
Author : Arthur H. Lefebvre
Publisher : CRC Press
Page : 420 pages
File Size : 55,8 Mb
Release : 1998-09-01
Category : Technology & Engineering
ISBN : 1560326735
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 : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 512 pages
File Size : 55,7 Mb
Release : 1945
Category : Aeronautics
ISBN : UIUC:30112008552223
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : Anonim
Publisher : Unknown
Page : 620 pages
File Size : 46,5 Mb
Release : 1945
Category : Aeronautics
ISBN : UIUC:30112108399095
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 516 pages
File Size : 43,8 Mb
Release : 1946
Category : Aeronautics
ISBN : CORNELL:31924089884468
Author : Jerrold D. Wear,Donald F. Schultz
Publisher : Unknown
Page : 60 pages
File Size : 49,8 Mb
Release : 1972
Category : Airplanes
ISBN : UIUC:30112106641696
Tests of various fuel nozzles were conducted with natural gas fuel in a full-annulus combustor. The nozzles were designed to provide either axial, angled, or radial fuel injection. Each fuel nozzle was evaluated by measuring combustion efficiency at relatively severe combustor operating conditions. Combustor blowout and altitude ignition tests were also used to evaluate nozzle designs. Results indicate that angled injection gave higher combustion efficiency, less tendency toward combustion instability, and altitude relight characteristics equal to or superior to those of the other fuel nozzles that were tested.
Author : Anonim
Publisher : Unknown
Page : 1212 pages
File Size : 48,7 Mb
Release : 1954
Category : Aeronautics
ISBN : UOM:39015024394291
Author : Jerrold D. Wear,Robert Ewing Jones
Publisher : Unknown
Page : 28 pages
File Size : 42,6 Mb
Release : 1973
Category : Airplanes
ISBN : UIUC:30112106885145