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Book Stability Limits and Efficiency of Swirl can Combustor Modules Burning Natural Gas Fuel  by Nicholas R  Marchionna

Download or read book Stability Limits and Efficiency of Swirl can Combustor Modules Burning Natural Gas Fuel by Nicholas R Marchionna written by Nicholas R. Marchionna and published by . This book was released on 1970 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1972
  • ISBN :
  • Pages : 402 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1972 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Jet Engine Exhaust Emissions of High altitude Commercial Aircraft Projected to 1990

Download or read book Jet Engine Exhaust Emissions of High altitude Commercial Aircraft Projected to 1990 written by Jack Grobman and published by . This book was released on 1974 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1970 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1974 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Fuel Distribution and Flame Stabilization Techniques on Combustion Stability Limits for Swirl can Combustor Modules Burning ASTM A1 Fuel

Download or read book Effect of Fuel Distribution and Flame Stabilization Techniques on Combustion Stability Limits for Swirl can Combustor Modules Burning ASTM A1 Fuel written by D. C. Briehl and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Combustion Stability of Single Swirl can Combustor Modules Using ASTM A1 Liquid Fuel

Download or read book Combustion Stability of Single Swirl can Combustor Modules Using ASTM A1 Liquid Fuel written by Richard W. Niedzwiecki and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel.

Book Comparison of Combustion Characteristics of ASTM A 1  Propane  and Natural gas Fuels in an Annular Turbojet Combustor

Download or read book Comparison of Combustion Characteristics of ASTM A 1 Propane and Natural gas Fuels in an Annular Turbojet Combustor written by Jerrold D. Wear and published by . This book was released on 1973 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA SP

    Book Details:
  • Author :
  • Publisher :
  • Release : 1970
  • ISBN :
  • Pages : 1166 pages

Download or read book NASA SP written by and published by . This book was released on 1970 with total page 1166 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Performance of a Modular Turbojet Combustor Burning Natural Gas Fuel

Download or read book Experimental Performance of a Modular Turbojet Combustor Burning Natural Gas Fuel written by Nicholas R. Marchionna and published by . This book was released on 1970 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cryogenic Information Report

Download or read book Cryogenic Information Report written by and published by . This book was released on 1970 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Engineering

Download or read book Aeronautical Engineering written by and published by . This book was released on 1971 with total page 976 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Book Stability Limits of a Methane fueled Swirl Combustor

Download or read book Stability Limits of a Methane fueled Swirl Combustor written by Daniel Thomas Martin and published by . This book was released on 1975 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Combustion Stability of Single Swirl can Combustor Modules Using ASTM A1 Liquid Fuel

Download or read book Combustion Stability of Single Swirl can Combustor Modules Using ASTM A1 Liquid Fuel written by Richard W. Niedzwiecki and published by . This book was released on 1969 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Ambient Conditions and Fuel Composition on Combustion Stability

Download or read book Effects of Ambient Conditions and Fuel Composition on Combustion Stability written by and published by . This book was released on 1997 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recent regulations on NO, emissions are promoting the use of lean premix (LPM) combustion for industrial gas turbines. LPM combustors avoid locally stoichiometric combustion by premixing fuel and the air upstream of the reaction region, thereby eliminating the high temperatures that produce thermal NO. Unfortunately, this style of combustor is prone to combustion oscillation. Significant pressure fluctuations can occur when variations in heat release periodically couple pressure to acoustic modes in the combustion chamber. These oscillations must be controlled because resulting vibration can shorten the life of engine hardware. Laboratory and engine field testing have shown that instability regimes can vary with environmental conditions. These observations prompted this study of the effects of ambient conditions and fuel composition on combustion stability. Tests are conducted on a sub-scale combustor burning natural gas, propane, and some hydrogen/hydrocarbon mixtures. A premix, swirl-stabilized fuel nozzle typical of industrial gas turbines is used. Experimental and numerical results describe how stability regions may shift as inlet air temperature, humidity, and fuel composition are altered. Results appear to indicate that shifting instability instability regimes are primarily caused by changes in reaction rate.