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Fundamentals of high lift for future...

Radespiel, Rolf.

Fundamentals of high lift for future civil aircraftcontributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Fundamentals of high lift for future civil aircraftedited by Rolf Radespiel, Richard Semaan.
Reminder of title:	contributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany /
other author:	Radespiel, Rolf.
Published:	Cham :Springer International Publishing :2021.
Description:	xii, 648 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Lift (Aerodynamics)
Online resource:	https://doi.org/10.1007/978-3-030-52429-6
ISBN:	9783030524296$q(electronic bk.)

Fundamentals of high lift for future civil aircraftcontributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany /
Fundamentals of high lift for future civil aircraftcontributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany /[electronic resource] :edited by Rolf Radespiel, Richard Semaan. - Cham :Springer International Publishing :2021. - xii, 648 p. :ill. (some col.), digital ;24 cm. - Notes on numerical fluid mechanics and multidisciplinary design,v.1451612-2909 ;. - Notes on numerical fluid mechanics and multidisciplinary design ;118..

Unconventional Applications and New Approaches for Flow Control -- A Brief Overview on Past Research on Coanda Assisted STOL Transport Aircraft -- Actuation system for Effective Flow Control of an Internally Blown Coanda flap -- Friction Drag Reduction by Transversal Spanwise Traveling Waves of Ribbed Surface -- Manipulation of Leading-Edge Vortex Flow -- Semi-Analytical Approach to the Determination of Free-Edge Stress Fields in Cylindrically Curved Composite Laminated Shells -- Air Curtain Flow Control for Aerodynamic Noise Reduction -- Multibody Modelling of an UHBR Engine and its Influence on the Dynamics of an Aircraft Wing.

This book reports on the latest numerical and experimental findings in the field of high-lift technologies. It covers interdisciplinary research subjects relating to scientific computing, aerodynamics, aeroacoustics, material sciences, aircraft structures, and flight mechanics. The respective chapters are based on papers presented at the Final Symposium of the Collaborative Research Center (CRC) 880, which was held on December 17-18, 2019 in Braunschweig, Germany. The conference and the research presented here were partly supported by the CRC 880 on "Fundamentals of High Lift for Future Civil Aircraft," funded by the DFG (German Research Foundation) The papers offer timely insights into high-lift technologies for short take-off and landing aircraft, with a special focus on aeroacoustics, efficient high-lift, flight dynamics, and aircraft design.

ISBN: 9783030524296$q(electronic bk.)

Standard No.: 10.1007/978-3-030-52429-6doiSubjects--Topical Terms:

809579
Lift (Aerodynamics)

LC Class. No.: TL574.L5 / F85 2021

Dewey Class. No.: 629.13233

Fundamentals of high lift for future civil aircraftcontributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany /
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520 $a This book reports on the latest numerical and experimental findings in the field of high-lift technologies. It covers interdisciplinary research subjects relating to scientific computing, aerodynamics, aeroacoustics, material sciences, aircraft structures, and flight mechanics. The respective chapters are based on papers presented at the Final Symposium of the Collaborative Research Center (CRC) 880, which was held on December 17-18, 2019 in Braunschweig, Germany. The conference and the research presented here were partly supported by the CRC 880 on "Fundamentals of High Lift for Future Civil Aircraft," funded by the DFG (German Research Foundation) The papers offer timely insights into high-lift technologies for short take-off and landing aircraft, with a special focus on aeroacoustics, efficient high-lift, flight dynamics, and aircraft design.
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