Leading-edge force features of the aerodynamic finite element method.
- 1 December 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (12), 864-867
- https://doi.org/10.2514/3.44344
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Application of Finite-Element Theory to Airplane ConfigurationsJournal of Aircraft, 1971
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- Spanwise distribution of induced drag in subsonic flow by the vortexlattice methodJournal of Aircraft, 1970
- On the singularity method of subsonic lifting- surface theoryJournal of Aircraft, 1969
- Analysis and design of wing-body combinations at subsonic and supersonic speeds.Journal of Aircraft, 1968