Fundamentals of High Lift for Future Civil Aircraft
portes grátis
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
Radespiel, Rolf; Semaan, Richard
Springer Nature Switzerland AG
10/2021
648
Mole
Inglês
9783030524319
15 a 20 dias
997
Descrição não disponível.
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.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
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
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.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
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
