Active Flow and Combustion Control 2014

Rudibert King

ISBN 10: 3319119664 / ISBN 13: 9783319119663

Verlag: Springer International Publishing, 2014

Beschreibung

Druck auf Anfrage Neuware - Printed after ordering - The book reports on the latest theoretical and experimental advances in the field of active flow and combustion control. It covers new developments in actuator technology and sensing, in robust and optimal open- and closed-loop control, as well as in model reduction for control. It collects contributions presented during the third edition of the Active Flow and Combustion Control conference, held in September 10-12, 2014 at the Technische Universität Berlin (Germany). This conference, as well as the research presented in the book, have been supported by the collaborative research center SFB 1029 -Substantial efficiency increase in gas turbines through direct use of coupled unsteady combustion and flow dynamics, funded by the DFG (German Research Foundation).

Bestandsnummer des Verkäufers 9783319119663

Bibliografische Details

• Titel: Active Flow and Combustion Control 2014
• Verlag: Springer International Publishing
• Erscheinungsjahr: 2014
• Sprache: Englisch
• ISBN-10: 3319119664
• ISBN-13: 9783319119663
• Einband: Buch
• Zustand: Neu
• Abmessungen: 241B x 160 H x 29 T Millimeter Breite: 241 mm, Höhe: 160 mm, Tiefe: 29 mm
• Gewicht: 805 Gramm

Über diesen Titel

Inhaltsangabe

The book reports on the latest theoretical and experimental advances in the field of active flow and combustion control. It covers new developments in actuator technology and sensing, in robust and optimal open- and closed-loop control, as well as in model reduction for control. It collects contributions presented during the third edition of the Active Flow and Combustion Control conference, held in September 10-12, 2014 at the Technische Universität Berlin (Germany). This conference, as well as the research presented in the book, have been supported by the collaborative research center SFB 1029 -Substantial efficiency increase in gas turbines through direct use of coupled unsteady combustion and flow dynamics, funded by the DFG (German Research Foundation).