Drag reduction by shock and boundary layer control : results of the project EUROSHOCK II, supported by the European Union, 1996-1999 / Egon Stanewsky, Jean Délery, John Fulker, and Paolo de Matteis (editors)
This volume contains a thorough description of the EU-supported project EUROSHOCK II concerned with the investigation of active shock and boundary layer control to improve aircraft performance. Discussed are basic experiments, supplemented by Navier-Stokes computations, to improve and validate physi...
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Full Text (via Springer) |
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| Format: | eBook |
| Language: | English |
| Published: |
Berlin :
Springer-Verlag,
2002.
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| Series: | Notes on numerical fluid mechanics and multidisciplinary design ;
v. 80. |
| Subjects: |
Table of Contents:
- Introduction
- The EUROSHOCK II project
- Modeling of active control phenomena
- Numerical simulation of airfoil and wing flow with control
- Airfoil and sheared-wing experiments with and without control
- Benefits of control application to aircraft wings/aircraft
- Assessment of shock and boundary layer control
- a summary
- Overall conclusions and future work
- Introduction to the individual contributions
- Study of control devices applied to a transonic shock wave/boundary layer interaction
- Hybrid and active control of shock wave
- Turbulent boundary layer interaction and perforated plate transpiration flow
- Active control of swept shock wave/boundary layer interactions
- Numerical investigation of active shock wave and boundary layer control on airfoils and sheared wings
- Boundary layer coupling to predict steady and unsteady transonic flows past an airfoil with and without shock control
- 2D numerical investigations of shock and boundary layer control techniques.