Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications

<div>Manufactured rotor-bearing system of the developed gas turbine: (a) compressor discs; (b) free turbine disc; and (c) locations of the bearings.</div>

Shock and Vibration

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Figure 3

Figure 3: Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications 

Figure 3 | Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications 