On the influence of the nozzle external configuration on the radiated screech and the decay of supersonic jets
The behaviour of screeching jets exhausting from an axisymmetric con-vergent-divergent nozzle was studied. The nozzle had a 2.9 mm throat diameter and a. 1.95 theoretical exit Mach number. Compressed nitrogen was used to obtain nozzle stagnation pressures from 0.15 to 1.4 MPa (absolute), i.e. condit...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institute of Fundamental Technological Research Polish Academy of Sciences
2016-03-01
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| Series: | Archives of Acoustics |
| Online Access: | https://acoustics.ippt.pan.pl/index.php/aa/article/view/3301 |
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