NASA: Controlling Combustion Instability

お客様の会社名: NASA Glenn Research Center, USA
発行日: Jan 2011

Ultra-low-emission combustors being developed for aircraft gas turbine engines are more susceptible to combustion instabilities. Caused by interaction between fluctuating heat release and naturally occurring acoustic resonances, these instabilities can shorten the life of the engine and result in premature mechanical failure.

  • 英語: NASA: Controlling Combustion Instability PDF, 286 KB
  • ドイツ語: NASA: Verbrennungsinstabilitäten kontrollieren PDF, 286 KB