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Drag Reduction by Shock and Boundary Layer Control : Results of the Project EUROSHOCK II. Supported by the European Union 1996¿1999 - Egon Stanewsky
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[EAN: 9783642077623], New book, [SC: 12.24], [PU: Springer Berlin Heidelberg], FLUIDMECHANICS; AIRCRAFTENGINES; AIRCRAFTWINGS; BOUNDARYLAYERS; FLOWCONTROL; MODELING; SHOCKWAVES; SIMULATIO… Plus…

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Editor: Stanewsky, Egon, Editor: Delery, J. Editor: Fulker, John, Editor: Matteis, Paolo de, Springer, Paperback, Auflage: Softcover reprint of hardcover 1st ed. 2002, 472 Seiten, Publizi… Plus…

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Drag Reduction by Shock and Boundary Layer Control Results of the Project EUROSHOCK II. Supported by the European Union 1996¿1999 - Stanewsky, Egon (Herausgeber); Matteis, Paolo de (Herausgeber); Fulker, John (Herausgeber); Delery, J. (Herausgeber)
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Drag Reduction by Shock and Boundary Layer Control Results of the Project EUROSHOCK II. Supported by the European Union 1996¿1999 - Livres de poche

2010, ISBN: 3642077625

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Données bibliographiques du meilleur livre correspondant

Détails sur le livre
Drag Reduction by Shock and Boundary Layer Control: Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 (Notes on Numerical ... and Multidisciplinary Design, 80, Band 80)

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.

Informations détaillées sur le livre - Drag Reduction by Shock and Boundary Layer Control: Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 (Notes on Numerical ... and Multidisciplinary Design, 80, Band 80)


EAN (ISBN-13): 9783642077623
ISBN (ISBN-10): 3642077625
Version reliée
Livre de poche
Date de parution: 2010
Editeur: Stanewsky, Egon, Springer Berlin Heidelberg
476 Pages
Poids: 0,715 kg
Langue: eng/Englisch

Livre dans la base de données depuis 2011-06-10T03:46:40+02:00 (Paris)
Page de détail modifiée en dernier sur 2023-11-21T22:29:52+01:00 (Paris)
ISBN/EAN: 3642077625

ISBN - Autres types d'écriture:
3-642-07762-5, 978-3-642-07762-3
Autres types d'écriture et termes associés:
Auteur du livre: matteis, mattei, fulk
Titre du livre: layer layer, she came drag, union, boundary, 1996


Données de l'éditeur

Auteur: Egon Stanewsky; J. Delery; John Fulker; Paolo de Matteis
Titre: 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
Editeur: Springer; Springer Berlin
452 Pages
Date de parution: 2010-12-04
Berlin; Heidelberg; DE
Imprimé / Fabriqué en
Langue: Anglais
213,99 € (DE)
219,99 € (AT)
236,00 CHF (CH)
POD
XX, 452 p.

BC; Hardcover, Softcover / Technik/Maschinenbau, Fertigungstechnik; Maschinenbau: Strömungsmechanik; Verstehen; Fluid mechanics; aircraft engines; aircraft wings; boundary layers; flow control; modeling; shock waves; simulation; transonic flow; Engineering Fluid Dynamics; Mechanical Engineering; Computational Intelligence; Solid Mechanics; Automotive Engineering; Multibody Systems and Mechanical Vibrations; Maschinenbau; Künstliche Intelligenz; Maschinenbau: Festkörpermechanik; Fahrzeugbau; BB; EA

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.
Covers shock control uniquely Sequel to NNFM 56

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9783540458562 Drag Reduction by Shock and Boundary Layer Control (J. Delery; John Fulker; Paolo de Matteis; Egon Stanewsky)


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