Development and Application of A High-Fidelity Numerical Tool for Dynamic Analysis of Bladed Disc Systems with Underplatform Dampers in Aircraft Engine Turbines

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

6 Citations (Scopus)
22 Downloads (Pure)

Fingerprint

Dive into the research topics of 'Development and Application of A High-Fidelity Numerical Tool for Dynamic Analysis of Bladed Disc Systems with Underplatform Dampers in Aircraft Engine Turbines'. Together they form a unique fingerprint.
Sort by

Keyphrases

Engineering