Implicit Finite-Difference Procedures for the Computation of Vortex Wakes
- 1 April 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (4), 581-590
- https://doi.org/10.2514/3.60663
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Experimental study of the effect of span loading on aircraft wakesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Vortex wakes behind high-lift wingsJournal of Aircraft, 1971
- The Method of Fractional StepsPublished by Springer Science and Business Media LLC ,1971
- A general formulation of alternating direction methodsNumerische Mathematik, 1964