Dynamic response of viscous-damped multi-shaft jet engines
Author:
Affiliation:
1. Pratt & Whitney Aircraft Division, United Aircraft Corporation, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44448
Reference12 articles.
1. A New Method of Calculating Natural Modes of Uncoupled Bending Vibration of Airplane Wings and Other Types of Beams
2. A General Method for Calculating Critical Speeds of Flexible Rotors
3. Gyroscopic Effects on the Critical Speeds of Flexible Rotors
4. Analysis for Calculating Lateral Vibration Characteristics of Rotating Systems With Any Number of Flexible Supports: Part 1—The Method of Analysis
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