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.
最新の技術開発動向をつかんで、イノベーションを加速。
メールマガジンの購読希望・変更/配信停止手続き