Aerodynamic Influence of Oscillating Adjacent Airfoils in a Linear Compressor Cascade
Author:
Affiliation:
1. Indian Institute of Technology, Kanpur, Kanpur 208 016, Uttar Pradesh, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055975
Reference27 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades
2. Blade Excitation by Aerodynamic Instabilities: A Compressor Blade Study
3. EXPERIMENTAL FLUTTER INVESTIGATIONS OF AN ANNULAR COMPRESSOR CASCADE: INFLUENCE OF REDUCED FREQUENCY ON STABILITY
4. Experimental Investigation of Mode Shape Sensitivity of an Oscillating Low-Pressure Turbine Cascade at Design and Off-Design Conditions
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