Supersonic laminar flow control on swept wings using distributed roughness
Authors:
- H. ReedHRH. Reed
- 14 January 2002
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- On the Secondary Instability of Three-Dimensional Boundary LayersTheoretical and Computational Fluid Dynamics, 2000
- Simulation of swept-wing vortices using nonlinear parabolized stability equationsJournal of Fluid Mechanics, 2000
- Secondary instability of crossflow vortices and swept-wing boundary-layer transitionJournal of Fluid Mechanics, 1999
- Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instabilityProgress in Aerospace Sciences, 1999
- Transition prediction and control for airplane applications1997
- On the stability of 3D boundary layers1997
- Laminar-turbulent transition in subsonic boundary layers - Research and applications in France1997
- Disturbance growth in an unstable three-dimensional boundary layer and its dependence on environmental conditionsJournal of Fluid Mechanics, 1996
- Nonlinear Crossflow Disturbances and Secondary Instabilities in Swept-Wing Boundary Layers1996
- Crossflow disturbances in three-dimensional boundary layers: nonlinear development, wave interaction and secondary instabilityJournal of Fluid Mechanics, 1994