Lifting Surface Theory of Axial Compressor Blade Rows: Part 11-Transonic Compressor
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (10) , 1372-1380
- https://doi.org/10.2514/3.49492
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Lifting Surface Theory of Axial Compressor Blade Rows: Part I-Subsonic CompressorAIAA Journal, 1974
- Three-dimensional vortex theory for axial compressor blade rows at subsonic and transonic speedsAIAA Journal, 1970
- Rotating pressure patterns in ducts: Their generation and transmissionJournal of Sound and Vibration, 1964
- The Transonic Flow Field of an Axial Compressor Blade RowJournal of the Aerospace Sciences, 1958