Time domain unsteady incompressible cascade airfoil theory for helicopter rotors in hover
- 1 March 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (3) , 257-267
- https://doi.org/10.2514/3.10107
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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