Gas Turbine Pollutant Emissions

Gas Turbine Pollutant Emissions

By: IMechE (Institution of Mechanical Engineers) (author)Hardback

Up to 2 WeeksUsually despatched within 2 weeks

Description

Emissions from civil subsonic air traffic are potentially in sufficient amounts to affect climate, particularly with the projected growth in air traffic. The main concern, which in the past was centred on air quality in the vicinity of airports, is now focused on the net global warming effects of emissions of oxides of nitrogen, carbon dioxide and contrails generated at altitude. The scientific debate is ongoing and engine manufacturers are studying a range of new low-emission and fuel-efficient technologies aimed at addressing all environmental concerns in a balanced manner. The large growth markets for both aero and stationary gas turbine continue to put pressure on the requirements to reduce combustion-generated pollutant emissions. The selection papers presented in "Gas Turbine Pollutant Emissions" provides opportunities for experts from industry, research associations, and academia to review and present current concerns and advances in technology. Topics covered include: legislation and control technology; the aero engine response to the protection of the global atmosphere; predictive methods for turbine combustor emissions; design and influence of swirl burners; and direct kinetic effects in turbulent flames. "Gas Turbine Pollutants Emissions" should be of value to research and design engineers and technology managers from both the aero and industrial gas turbine industry, as well as researchers from universities and independent research laboratories.

About Author

The IMechE is the United Kingdom's qualifying body for mechanical engineers and the home of mechanical engineers for over 150 years. Around 75,000 engineers world-wide are members.

Contents

Aircraft gas turbine emissions -legislation and control technology, B. Jones; improved combustor turndown using a variable swirl number fuel injector, K.D. Brundish and C.W. Wilson; the aero engine response to the projection of the global atmosphere, M.J.R. Le Dilosquer; predictive methods for gas turbine combustor emissions, J.B. Moss; the influence of premixture equivalence ratio on the thermo-acoustic response of a swirl burner, C.J. Lawn; the modelling of CO and NO foundation in turbulent jet flames, R.P. Lindstedt and E.M. Vaos.

Product Details

  • ISBN13: 9781860583155
  • Format: Hardback
  • Number Of Pages: 96
  • ID: 9781860583155
  • weight: 404
  • ISBN10: 1860583156

Delivery Information

  • Saver Delivery: Yes
  • 1st Class Delivery: Yes
  • Courier Delivery: Yes
  • Store Delivery: Yes

Prices are for internet purchases only. Prices and availability in WHSmith Stores may vary significantly

Close