Drag Reduction by Shock and Boundary Layer Control : Results of the Project Euroshock II Supported by the European Union, 1996-1999

Stanewsky, Egon (EDT); Delery, Jean (EDT); Fulker, John (EDT); Matteis, Paolo De (EDT)

ISBN 10: 3540433171 / ISBN 13: 9783540433170

Published by Springer, 2002

About this Item

Seller Inventory # 916399-n

Bibliographic Details

• Title: Drag Reduction by Shock and Boundary Layer Control : Results of the Project Euroshock II Supported by the European Union, 1996-1999
• Publisher: Springer
• Publication Date: 2002
• Language: English
• ISBN 10: 3540433171
• ISBN 13: 9783540433170
• Binding: Hardcover
• Condition: New

About this title

Synopsis

The survival of the Aeronautical Industries of Europe in the highly competitive World Aviation Market is strongly dependent on such factors as time-to-market of a new or derivative aircraft and on its manufacturing costs but also on the achievement of a competitive technological advantage by which an increased market share can be gained. Recognizing this, cooperative research is continuously encouraged and co-financed by the European Union in order to strengthen the scientific and technological base of the Aeronautical Industries thus providing - among others - the technological edge needed for survival. Corresponding targets of research within Area 3, Technologies for Transport Means, and here in particular Area 3A, Aeronautics Technologies, of the Industrial and Materials Technologies Program ( Brite -EuRam III, 1994 -1998) have been identified to be aircraft efficiency, cost effectiveness and environmental impact. Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10%, a reduction in aircraft fuel consumption of 30%, and a reduction in airframe, engine and system weight of 20% are envisaged. Meeting these objectives has, of course, also a strong positive impact on the environment.

From the Back Cover

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.