A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic Flows
- 1 September 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (9) , 544-560
- https://doi.org/10.2514/8.7780
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic FlowsJournal of the Aerospace Sciences, 1958
- The asymptotic solution of linear differential equations of the second order for large values of a parameterPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1954