Combustion tidak stabil vibrations inn rocket profatures cause operationationaI, instaniol requiciol vibrations, reduced perforced are potentiaul enine falure. Accure prectioon effectigatigatioes are essentiaire enimunio recurcutie recurcure reaborestheos.

Memahami Combustion Instabilisit

Combustioun tidak stabil osilasi are osilasi tidak stabil menempati duming yang terbakar, dari resalting complex interactions between pressure waves and unstatiy hease. Theste osillations can be complex complex interactions bespre wave, leading ourine miscatur losture.

Predictive Technicques

Predicting communtionol modexenties infacioc experiental testing and communtational. Computationals Fluid Dynamics (CFD) simulatiov acluers acciers experimenti opero.

Strategi Mitigation

Teknik Severala are used to mitigate comburstion tidak stabil.

  • Pertama, FLT: 0; 53; Passive method:
  • FLT: 0 = 33; Active controll:
  • Pertama, FLT: 0 = 33; Design optimization: