Aeroelastically deflecting flaps for shock/boundary-layer interaction control
- 1 June 2003
- journal article
- Published by Elsevier BV in Journal of Fluids and Structures
- Vol. 17 (7), 1001-1016
- https://doi.org/10.1016/s0889-9746(03)00053-7
Abstract
No abstract availableKeywords
This publication has 16 references indexed in Scilit:
- Simulation and experimental analysis of a novel SBLI flow control systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Smart mesoflaps for control of shock boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Experimental study of mesoflaps for SBLI controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing techniquePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- A method for separating shock wave motion and turbulence in LDV measurementsExperiments in Fluids, 1999
- Study of Passive Control in a Transonic Shock Wave/Boundary-Layer InteractionAIAA Journal, 1998
- Supersonic-inlet boundary-layer bleed flowAIAA Journal, 1996
- Shock-wave/boundary-layer interactions with bleed. I - Effect of slot angleJournal of Propulsion and Power, 1995
- An investigation of LDV velocity bias correction techniques for high-speed separated flowsExperiments in Fluids, 1993
- Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interactionAIAA Journal, 1992