Fundamentals of high lift for future civil aircraft : contributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany / Rolf Radespiel, Richard Semaan (eds.).
2021
TL574.L5
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Title
Fundamentals of high lift for future civil aircraft : contributions to the final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany / Rolf Radespiel, Richard Semaan (eds.).
ISBN
9783030524296 (electronic bk.)
3030524299 (electronic bk.)
3030524280
9783030524289
3030524299 (electronic bk.)
3030524280
9783030524289
Published
Cham : Springer, 2021.
Language
English
Description
1 online resource (xii, 648 pages) : illustrations (some color)
Item Number
10.1007/978-3-030-52429-6 doi
Call Number
TL574.L5
Dewey Decimal Classification
629.132/33
620.1064
620.1064
Summary
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
Bibliography, etc. Note
Includes bibliographical references.
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Access limited to authorized users.
Digital File Characteristics
text file
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Series
Notes on numerical fluid mechanics and multidisciplinary design ; 145. 1612-2909
Available in Other Form
3030524280
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Table of Contents
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.
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.