doerffer (95 resultados)

Condición: Gut. 11 Seiten mit zahlr. Ill. Der hier angebotene Sonderdruck ist informativ und kurz gehalten. Er stammt aus der Separaten-Sammlung einer wissenschaftlichen Bibliothek und trägt einen den Text nicht verdeckenden Stempel. Insgesamt ordentlicher Erhaltungszustand. ENGLISCH; Aufgrund der Rarität und des geringen Umfangs des Werkes bitten wir um Verständnis, dass dieser Sonderdruck vom Rückgaberecht ausgeschlossen ist. Sprache: Englisch Gewicht in Gramm: 40.

Condición: As New. Unread book in perfect condition.

Taschenbuch. Condición: Gut. 112 Seiten. 270x185 mm Das Buch befindet sich im einwandfreien Zustand. BSG396 Sprache: Englisch Gewicht in Gramm: 203.

Paperback. Condición: New.

Taschenbuch. Condición: Neu. Gebraucht - Wie neu Unbenutzt, unauffällig als Remittende gekennzeichnet. Schnelle Lieferung, Kartonverpackung. Abzugsfähige Rechnung. Bei Mehrfachbestellung werden die Versandkosten anteilig erstattet. -Some compare the evolving Web to the revolution of the Gutenberg press. How does the Web shape the role and understanding of leadership What are key challenges and opportunities What mindsets, skills and knowledge are necessary 'The Leadership Implications of the Evolving Web,' provides and analyzes over 300 pioneer examples from the private, public and non-profit sector in Germany, Europe and the US. A new leadership paradigm seems to be emerging with an inexorable shift away from one-way, hierarchical, organization-centric communication toward two-way, network-centric, participatory, and collaborative leadership styles. Which requirements and trends, which opportunities and key challenges are emerging for leadership Aim of the study is to enable managers from all sectors to anticipate changes and proactively take advantage of opportunities that are emerging. ?Target group for this publication are people in leadership positions in organizations across all sectors from managers in executive and supervisory boards, operations, human resources to academics and practitioners, advisers and policymakers.? The Study "Leadership & Web 2.0" has been presented by authors Grady McGonagill, ED and Tina Doerffer, MPA amongst others at the International Leadership Academy in Boston (2010). 174 pp. Englisch.

VIII, 540 p. Hardcover. Versand aus Deutschland / We dispatch from Germany via Air Mail. Einband bestoßen, daher Mängelexemplar gestempelt, sonst sehr guter Zustand. Imperfect copy due to slightly bumped cover, apart from this in very good condition. Stamped. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 144. Sprache: Englisch.

xi, 511 p. Hardcover. Versand aus Deutschland / We dispatch from Germany via Air Mail. Einband bestoßen, daher Mängelexemplar gestempelt, sonst sehr guter Zustand. Imperfect copy due to slightly bumped cover, apart from this in very good condition. Stamped. Sprache: Englisch.

Condición: New.

Perfect Paperback. Condición: New.

Condición: New.

Condición: As New. Unread book in perfect condition.

85 Seiten, Normalformat, 8°, Broschur. Gebrauchsspuren.

Hardcover. Condición: new. Hardcover. This open-access book reports on both experimental and numerical findings from the H2020-funded project TEAMAero (Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications). It covers novel contributions on improving the fundamental understanding of the physics of shock wave boundary layer interaction, developments in ow control for mitigation of shock effects, and advanced numerical methods for predicting those effects. All in all, this book offers a timely snapshot of research and developments in numerical methods for flow analysis and control, with a special emphasis on high-speed flows. It offers extensive information to both researchers and professionals. It covers novel contributions on improving the fundamental understanding of the physics of shock wave boundary layer interaction, developments in ow control for mitigation of shock effects, and advanced numerical methods for predicting those effects. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.

Condición: Gut. 105 Seiten mit zahlr. Ill., 1 Tafel mit farb. Abb. Der hier angebotene Sonderdruck stammt aus der Separaten-Sammlung einer wissenschaftlichen Bibliothek und trägt einen den Text nicht verdeckenden Stempel. Insgesamt ordentlicher Erhaltungszustand. Sprache: Deutsch Gewicht in Gramm: 200.

Taschenbuch. Condición: Gut. 112 Seiten. 270x185 mm Die Kanten des Buches sind etwas berieben. Ansonsten befindet sich das Buch im guten Zustand. BSG383 Sprache: Deutsch Gewicht in Gramm: 251.

Hardcover. Condición: Very Good. Text clean and unmarked. Binding tight. Boards have light wear. Edges of pages have light wear. Name written on front free end paper.

Condición: Brand New. New. US edition. Expediting shipping for all USA and Europe orders excluding PO Box. Excellent Customer Service.

Hardcover. Condición: Brand New. 380 pages. 9.25x6.10x9.49 inches. In Stock.

Condición: Hervorragend. Zustand: Hervorragend | Seiten: 171 | Sprache: Englisch | Produktart: Bücher | Keine Beschreibung verfügbar.

Buch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - This open-access book reports on both experimental and numerical findings from the H2020-funded project TEAMAero (Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications). It covers novel contributions on improving thefundamental understanding of the physics of shock wave boundary layer interaction, developments in ow control for mitigation ofshock effects, and advanced numerical methods for predicting those effects. All in all, this book offers a timely snapshot of research and developments in numerical methods for flow analysis and control, with a special emphasis on high-speed flows. It offers extensive information to both researchers and professionals.

Condición: New. In.

Condición: New.

Taschenbuch. Condición: Neu. Transition Location Effect on Shock Wave Boundary Layer Interaction | Experimental and Numerical Findings from the TFAST Project | Piotr Doerffer (u. a.) | Taschenbuch | viii | Englisch | 2021 | Springer International Publishing | EAN 9783030474638 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.

Condición: Hervorragend. Zustand: Hervorragend | Seiten: 548 | Sprache: Englisch | Produktart: Bücher | Keine Beschreibung verfügbar.

Taschenbuch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.

Buch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction. The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project. The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.

Taschenbuch. Condición: Neu. Neuware -This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction.The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project.The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 548 pp. Englisch.

Buch. Condición: Neu. Neuware -This book presents experimental and numerical findings on reducing shock-induced separation by applying transition upstream the shock wave. The purpose is to find out how close to the shock wave the transition should be located in order to obtain favorable turbulent boundary layer interaction.The book shares findings obtained using advanced flow measurement methods and concerning e.g. the transition location, boundary layer characteristics, and the detection of shock wave configurations. It includes a number of experimental case studies and CFD simulations that offer valuable insights into the flow structure. It covers RANS/URANS methods for the experimental test section design, as well as more advanced techniques, such as LES, hybrid methods and DNS for studying the transition and shock wave interaction in detail. The experimental and numerical investigations presented here were conducted by sixteen different partners in the context of the TFAST Project.The general focus is on determining if and how it is possible to improve flow performance in comparison to laminar interaction. The book mainly addresses academics and professionals whose work involves the aerodynamics of internal and external flows, as well as experimentalists working with compressible flows. It will also be of benefit for CFD developers and users, and for students of aviation and propulsion systems alike.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 548 pp. Englisch.

Condición: New. In.

Condición: New. In.