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Egon Stanewsky; J. Delery; John Fulker; Paolo de Matteis:
Drag Reduction by Shock and Boundary Layer Control - neues BuchISBN: 9783540458562
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 aircra… Mehr…
ISBN: 9783540458562
*Drag Reduction by Shock and Boundary Layer Control* - Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 / pdf eBook für 213.99 € / Aus dem Bereich: eBooks, S… Mehr…
Drag Reduction by Shock and Boundary Layer Control - neues Buch
2013, ISBN: 9783540458562
Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999, eBook Download (PDF), eBooks, [PU: Springer Berlin Heidelberg]
ISBN: 9783540458562
Drag Reduction by Shock and Boundary Layer Control ab 324.49 EURO Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 Medien > Bücher, [PU: Springer, Berlin/Hei… Mehr…
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Detailangaben zum Buch - Drag Reduction by Shock and Boundary Layer Control
EAN (ISBN-13): 9783540458562
Erscheinungsjahr: 2013
Herausgeber: Springer Berlin Heidelberg
Buch in der Datenbank seit 2017-05-10T02:54:14+02:00 (Berlin)
Detailseite zuletzt geändert am 2023-11-01T13:31:19+01:00 (Berlin)
ISBN/EAN: 9783540458562
ISBN - alternative Schreibweisen:
978-3-540-45856-2
Alternative Schreibweisen und verwandte Suchbegriffe:
Autor des Buches: mattei, friedemann
Titel des Buches: boundary layer, shock shock
Daten vom Verlag:
Autor/in: Egon Stanewsky; J. Delery; John Fulker; Paolo de Matteis
Titel: 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
Verlag: Springer; Springer Berlin
452 Seiten
Erscheinungsjahr: 2013-11-11
Berlin; Heidelberg; DE
Sprache: Englisch
213,99 € (DE)
220,00 € (AT)
236,00 CHF (CH)
Available
XX, 452 p.
EA; E107; eBook; Nonbooks, PBS / Technik/Maschinenbau, Fertigungstechnik; Maschinenbau: Strömungsmechanik; Verstehen; Fluid mechanics; aircraft engines; aircraft wings; boundary layers; flow control; modeling; shock waves; simulation; transonic flow; C; Engineering Fluid Dynamics; Mechanical Engineering; Computational Intelligence; Solid Mechanics; Automotive Engineering; Multibody Systems and Mechanical Vibrations; Engineering; Maschinenbau; Künstliche Intelligenz; Maschinenbau: Festkörpermechanik; Fahrzeugbau; BC
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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