Numerical Investigation of a Bias-Flow Perforated Liner for Damping of Thermoacoustic Instabilities.
Similar Items:
1
Conference Proceedings
Numerical Investigation of a Bias-Flow Perforated Liner for Damping of Thermoacoustic Instabilities
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Comparison of Experimental and Numerical Results Concerning the Damping of Perforated Liners with Bias Flow.
American Society of Mechanical Engineers |
9
Technical Paper
Numerical Study of Flow Structure and Thrust Performance for 3-D MEMS-based Nozzles.
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Experimental Investigation of the Acoustic Damping of Perforated Liners with Bias Flow
American Institute of Aeronautics and Astronautics |
10
Technical Paper
The application of a time-domain model to investigate the impedance of perforate liners including the effects of bias flow
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Experimental and Numerical Investigation of Aerodynamic Flow Control Using Oscillating Adaptive Surfaces.
American Institute of Aeronautics and Astronautics |