Aeroelastic Response in an Oscillating Transonic Compressor Cascade—An Experimental and Numerical Approach
The steady-state aerodynamics and the aeroelastic response have been analyzed in an oscillating linear transonic cascade at the KTH Royal Institute of Technology. The investigated operating points (<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inli...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-04-01
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| Series: | International Journal of Turbomachinery, Propulsion and Power |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2504-186X/10/2/7 |
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