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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 de Rolf Radespiel

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: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, cartea 145

Editat de Rolf Radespiel, Richard Semaan
en Limba Engleză Paperback – 18 oct 2021
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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Specificații

ISBN-13: 9783030524319
ISBN-10: 3030524310
Ilustrații: XII, 648 p. 404 illus., 301 illus. in color.
Dimensiuni: 155 x 235 mm
Greutate: 0.91 kg
Ediția:1st ed. 2021
Editura: Springer International Publishing
Colecția Springer
Seria Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Locul publicării:Cham, Switzerland

Cuprins

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.

Textul de pe ultima copertă

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.
 

Caracteristici

Reports on numerical and experimental findings concerning aeroacoustics, efficient high-lift, and flight dynamics Places special emphasis on short take-off and landing aircraft applications Covers multidisciplinary aspects of aircraft design