Unsteady Flow in a Supersonic Cascade with Subsonic Leading-Edge Locus
- 1 December 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 16 (12) , 1248-1254
- https://doi.org/10.2514/3.61040
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Unsteady flow in a supersonic cascade with strong in-passage shocksJournal of Fluid Mechanics, 1977
- Further Developments in the Aerodynamic Analysis of Unsteady Supersonic Cascades—Part 1: The Unsteady Pressure FieldJournal of Engineering for Power, 1977
- On the issue of resonance in an unsteady supersonic cascadeAIAA Journal, 1975
- Cascade with Subsonic Leading-Edge LocusAIAA Journal, 1975
- The unsteady supersonic cascade in subsonic axial flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- On the Unsteady Supersonic Cascade With a Subsonic Leading Edge—An Exact First Order Theory—Part 1Journal of Engineering for Power, 1974
- The Unsteady Aerodynamics of a Finite Supersonic Cascade With Subsonic Axial FlowJournal of Applied Mechanics, 1973
- Sound transmission through bladeJournal of Sound and Vibration, 1970
- System Mode Shapes in the Flutter of Compressor Blade RowsJournal of the Aeronautical Sciences, 1956