Slender wing rock revisited
- 1 May 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 30 (3) , 352-356
- https://doi.org/10.2514/3.46341
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Sources of High Alpha Vortex Asymmetry at Zero SideslipJournal of Aircraft, 1992
- Experimental investigations of the vortex flow on delta wings at high incidenceAIAA Journal, 1992
- Rapid prediction of high-alpha unsteady aerodynamics of slender-wingaircraftJournal of Aircraft, 1992
- Symmetric and asymmetric vortex flows at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- An experimental study of the nonlinear dynamic phenomenon known as wing rockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Flow visualization study of delta wings in wing-rock motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Analytic prediction of the maximum amplitude of slender wing rockJournal of Aircraft, 1989
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Similarity in Vortex Asymmetries over Slender Bodies and WingsAIAA Journal, 1977
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971