A compressible three‐dimensional design method for radial and mixed flow turbomachinery blades
- 5 September 1991
- journal article
- research article
- Published by Wiley in International Journal for Numerical Methods in Fluids
- Vol. 13 (5), 599-624
- https://doi.org/10.1002/fld.1650130505
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Application of Viscous Flow Computations for the Aerodynamic Performance of a Backswept Impeller at Various Operating ConditionsJournal of Turbomachinery, 1988
- A design method for two-dimensional cascades of turbomachinery bladesInternational Journal for Numerical Methods in Fluids, 1987
- Theory of Blade Design for Large Deflections: Part II—Annular CascadesJournal of Engineering for Gas Turbines and Power, 1984
- Theory of Blade Design for Large Deflections: Part I—Two-Dimensional CascadeJournal of Engineering for Gas Turbines and Power, 1984
- An Improved Time-Marching Method for Turbomachinery Flow CalculationJournal of Engineering for Power, 1983
- An Inverse Time Marching Method for the Definition of Cascade GeometryJournal of Engineering for Power, 1982
- A Method for Inverse Aerofoil and Cascade Design by Surface VorticityPublished by ASME International ,1982
- Multi-level adaptive solutions to boundary-value problemsMathematics of Computation, 1977
- Lifting-surface theory of straight cascades of swept bladesInternational Journal of Mechanical Sciences, 1976
- Sweep and Dihedral Effects in Axial-Flow TurbomachineryJournal of Basic Engineering, 1963