Del i serien Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Drag Reduction by Shock and Boundary Layer Control

Results of the Project EUROSHOCK II. Supported by the European Union 1996–1999

Häftad, Engelska, 2010

AvEgon Stanewsky,J. Delery,John Fulker,Paolo de Matteis

2 749 kr

Beställningsvara. Skickas inom 10-15 vardagar. Fri frakt för medlemmar vid köp för minst 249 kr.

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 physical models relevant to control and the extension, validation and application of various computational methods to airfoil and wing flows with control. Furthermore described are experiments on airfoils and wings carried out to assess the aerodynamic benefits of control and to provide data for validation purposes. Finally, control applications to real aircraft and the corresponding installation penalties and mission benefits are addressed. This volume is a sequel to Vol. 56 on passive shock control.

Produktinformation

Utgivningsdatum2010-12-04
Mått155 x 235 x 26 mm
Vikt715 g
FormatHäftad
SpråkEngelska
SerieNotes on Numerical Fluid Mechanics and Multidisciplinary Design
Antal sidor452
FörlagSpringer-Verlag Berlin and Heidelberg GmbH & Co. KG
ISBN9783642077623

Tillhör följande kategorier

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.