Similarity relation for vortex-asymmetry onset on slender pointed forebodies
- 1 April 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (4) , 559-561
- https://doi.org/10.2514/3.7929
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender VehiclesJournal of Spacecraft and Rockets, 1981
- Similarity in Vortex Asymmetries over Slender Bodies and WingsAIAA Journal, 1977
- Half- and Full-Model Experiments on Slender Cones at Angle of AttackJournal of Spacecraft and Rockets, 1973
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- The Calculation of Three-Dimensional Turbulent Boundary Layers: Part I: Flow over the Rear of an Infinite Swept WingAeronautical Quarterly, 1967
- The boundary layer of a class of infinite yawed cylindersMathematical Proceedings of the Cambridge Philosophical Society, 1950
- The Boundary Layer of Yawed CylindersJournal of the Aeronautical Sciences, 1948