Drag Reduction by Shock and Boundary Layer Control - Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 (Hardcover, 2002 ed.)

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.

General

Imprint:	Springer-Verlag
Country of origin:	Germany
Series:	Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 80
Release date:	2001
First published:	2002
Editors:	Egon Stanewsky • J. Delery • John Fulker • Paolo De Matteis
Dimensions:	235 x 155 x 26mm (L x W x T)
Format:	Hardcover
Pages:	452
Edition:	2002 ed.
ISBN-13:	978-3-540-43317-0
Categories:	Books > Professional & Technical > Mechanical engineering & materials > Materials science > Mechanics of fluids > Aerodynamics
LSN:	3-540-43317-1
Barcode:	9783540433170

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