Validation of a Methodology to Assess the Flutter Limit-Cycle Oscillation Amplitude of Low-Pressure Turbine Bladed Disks—Part I: Mach Number Effects
Year: 2024
Type: article
DOI: 10.1115/1.4066587
Institution: Universidad Politécnica de Madrid
Language: English
Subfield: Civil and Structural Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G1725385510, G782596663
OpenAlex ID: W4402634359
