Drag Reduction by Shock and Boundary Layer Control
Springer Berlin (Verlag)
978-3-642-07762-3 (ISBN)
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.
Erscheint lt. Verlag | 4.12.2010 |
---|---|
Reihe/Serie | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
Zusatzinfo | XX, 452 p. |
Verlagsort | Berlin |
Sprache | englisch |
Maße | 155 x 235 mm |
Gewicht | 715 g |
Themenwelt | Technik ► Maschinenbau |
Schlagworte | aircraft engines • aircraft wings • boundary layers • flow control • fluid mechanics • Modeling • Shock waves • Simulation • transonic flow |
ISBN-10 | 3-642-07762-5 / 3642077625 |
ISBN-13 | 978-3-642-07762-3 / 9783642077623 |
Zustand | Neuware |
Haben Sie eine Frage zum Produkt? |
aus dem Bereich