Periodicity, Superposition, and 3D Effects in Supersonic Compressor Flutter Aerodynamics

Articles in the same Issue

1. CONTENTS
2. Analysis of Transonic Flow Through a Lightly Loaded Compressor Rotor
3. Atomization Under Engine-Burner Cross-Flow Conditions
4. Inter and Intra Blade Row Laser Velocimetry Studies of Gas Turbine Compressor Flows
5. Characteristics of Liquid Hydrogen Fueled Supersonic Aircraft Engine
6. Aerodynamically forced Response of an Airfoil Including Profile and Incidence Effects
7. Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions
8. Experimental and Theoretical Study on Liquid Atomization into a Gas Stream
9. Friction Damping of Random Vibration in Gas Turbine Engine Airfoils
10. Calculation of Confined Swirling Flows
11. A Variation Finite Element Method for Solving the Blade-to-Blade Flow in Centrifugal Compressor's Cascades with Splitter Blades on an Arbitrary Streamsheet of Revolution and a Mathematical Treatment to the Region Behind Cascades
12. Numerical Integration of the 3D Unsteady Euler Equations for Flutter Analysis of Axial Flow Compressors
13. Periodicity, Superposition, and 3D Effects in Supersonic Compressor Flutter Aerodynamics