A multivortex method for axisymmetric bodies at angle of attack.
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (12) , 959-966
- https://doi.org/10.2514/3.44317
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Effects of vortex separation on the lift distribution on bodies of elliptic cross sectionJournal of Aircraft, 1969
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- Flow separation about elliptic cones at incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965