Fundamentals of High Lift for Future Civil Aircraft, 1st ed. 2021 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 Series, Vol. 145
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.
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.
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
Date de parution : 10-2021
Ouvrage de 648 p.
15.5x23.5 cm
Date de parution : 10-2020
Ouvrage de 648 p.
15.5x23.5 cm
Thèmes de Fundamentals of High Lift for Future Civil Aircraft :
Mots-clés :
Trailing-edge Noise Reduction; STOL Aircraft Concept; Flow Simulation of Porous Material; Cabin Noise Prediction; Droop Nose Design; Compact Electrical Compressors; Active High-Lift Sensors and Actuators; Ultra High Bypass Ratio Engines; Aircraft Flight Control; Aeroelasticity; Uncertainty Quantification and Propagation; CRC 880
