This work conducts numerical studies of impinging jet acoustics in support of the efforts to suppress high nonlinear acoustic loads on the spacecraft structures during the launch phase.
Project Details
The focus is on using high-accuracy analysis to understand the appearance of the acoustic feedback loops and means of the effective noise control.
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Research Team
Principal Investigators
CO-Investigators
Reda R. Mankbadi
Distinguished Professor
- Aerospace Engineering Department
- Daytona College of Engineering
Reda R. Mankbadi
Distinguished Professor
- Aerospace Engineering Department
- Daytona College of Engineering