Reduced-Order Modeling of Unsteady Viscous Flow in a Compressor Cascade
- 1 June 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 36 (6), 1039-1048
- https://doi.org/10.2514/2.477
Abstract
No abstract availableThis publication has 28 references indexed in Scilit:
- A Framework for Analyzing the Dynamics of Flexibly-Bladed TurbomachinesPublished by ASME International ,1996
- Eigenvalue calculation procedure for an Euler/Navier-Stokes solver with application to flows over airfoilsJournal of Computational Physics, 1991
- Modified exponential series approximation for the Theodorsen functionJournal of Aircraft, 1991
- Consistent rational-function approximation for unsteady aerodynamicsJournal of Aircraft, 1991
- Improved exponential time series approximation of unsteady aerodynamic operatorsJournal of Aircraft, 1988
- A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of EquationsJournal of Engineering for Gas Turbines and Power, 1986
- Supersonic Stall Flutter of High-Speed FansJournal of Engineering for Power, 1982
- Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System ModelJournal of Engineering for Power, 1976
- Cascade Flutter in Compressible FlowTransactions of the Japan Society of Mechanical Engineers, 1972
- Vibration of Cascade Blades Treated by Actuator Disc MethodsProceedings of the Institution of Mechanical Engineers, 1959