Role of Filament Strain in the Free-Vortex Modeling of Rotor Wakes
- 1 April 2004
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 49 (2), 176-191
- https://doi.org/10.4050/jahs.49.176
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Technical Note: Accuracy of Straight-Line Segmentation Applied to Curvilinear Vortex FilamentsJournal of the American Helicopter Society, 2001
- Stability, Consistency and Convergence of Time-Marching Free-Vortex Rotor Wake AlgorithmsJournal of the American Helicopter Society, 2001
- Viscous Vortex MethodsPublished by Cambridge University Press (CUP) ,2000
- Correlation of Helicopter Rotor Tip Vortex MeasurementsAIAA Journal, 2000
- Rotor Free‐Wake Modeling Using a Pseudo‐Implicit Technique — Including Comparisons with Experimental DataJournal of the American Helicopter Society, 1995
- Flow visualization of compressible vortex structures using density gradient techniquesExperiments in Fluids, 1993
- A new method for improved rotor free-wake convergencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Correlation of turbulent trailing vortex decay dataJournal of Aircraft, 1976
- Numerical study of slightly viscous flowJournal of Fluid Mechanics, 1973
- The Growth of a Vortex in Turbulent FlowAeronautical Quarterly, 1965