Propagation of Stall in a Compressor Blade Row
- 1 August 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (8) , 541-554
- https://doi.org/10.2514/8.3395
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Some Stall and Surge Phenomena in Axial-Flow CompressorsJournal of the Aeronautical Sciences, 1953
- On Asymmetric Flow in an Axial-Flow Compressor StageJournal of Applied Mechanics, 1953