Lifting Surface Theory of Axial Compressor Blade Rows: Part I-Subsonic Compressor
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (10) , 1363-1372
- https://doi.org/10.2514/3.49491
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic FlowsJournal of the Aerospace Sciences, 1958
- On the Vortex Theory of the Screw PropellerJournal of the Aeronautical Sciences, 1937
- On the vortex theory of screw propellersProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1929