NASA Glenn Research Center, USA |
|
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.
Faire avancer l'innovation. Toujours à la pointe de l'évolution technologique.
S’abonner à nos newsletters, gérer ses abonnements ou se désabonner. La newsletter mensuelle contenant toutes les informations liées à l’aéronautique et défense.