Development of a stationary crossflow vortices on a swept wing
Authors:
- 20 June 1994
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 23 references indexed in Scilit:
- Instability Features Appearing on Swept Wing Configurations1990
- An Evaluation of Stability-Based Methods for Transition of Three-Dimensional Flows1990
- Experimental and Theoretical Analysis of Natural Transition on “Infinite” Swept Wing1990
- Stability of Three-Dimensional Boundary LayersAnnual Review of Fluid Mechanics, 1989
- The boundary-layer transition on rotating cones in axial flow with free-stream turbulence.JSME International Journal, 1987
- Flow structures formed by axisymmetric spinning bodiesAIAA Journal, 1985
- Some observations of the transition process on the windward face of a long yawed cylinderJournal of Fluid Mechanics, 1985
- Boundary-layer transition on a rotating cone in axial flowJournal of Fluid Mechanics, 1983
- Compressible laminar boundary layers with suction on swept and tapered wingsJournal of Aircraft, 1977
- On the stability of three-dimensional boundary layers with application to the flow due to a rotating diskPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1955