Spanwise distribution of induced drag in subsonic flow by the vortexlattice method
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 7 (6) , 574-576
- https://doi.org/10.2514/3.44219
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- On the singularity method of subsonic lifting- surface theoryJournal of Aircraft, 1969
- Correlation of the vortex lattice method on rotor/wing configurations.Journal of Aircraft, 1969
- Some Remarks on Vortex Drag and its Spanwise Distribution in Incompressible FlowThe Aeronautical Journal, 1968
- The Theory of Thin Wings in Subsonic FlowPublished by Springer Nature ,1967