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Research
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Clusters of Excellence at TU Braunschweig
SE²A - Sustainable and Energy-Efficient Aviation
Research
ICA B "Flight Physics and Vehicle Systems"
JRP - Permeation assessment for cryogenic applications by means of Fiber Bragg Grating sensors
ICA B "Flight Physics and Vehicle Systems"
B5.2 - Application of physics-based finite-element tools in stiffness tailored structures for cryogenic hydrogen storage for improved mechanical and thermo-mechanical response
B4.2 - Consistent Multilevel Model Coupling and Knowledge Representation in Multidisciplinary Analysis and Design
B4.1- Collaborative Multidisciplinary Structural Design and Thermal Management for Electric Aircraft
B3.5 - Production technologies for hybrid suction designs - Bonding of micro-perforated sheets for hybrid laminar flow control suction panels
B3.2 - Advancing the additive xHLFC suction panel concept towards wind-tunnel readiness
B3.1 - Protective, multifunctional suction shells for hybrid laminar flow control: Design, integration, simulation and testing
B2.5 - EverScale - Enhancement and verification of load alleviation technologies by subscale flight testing
B2.4- Hybrid load alleviation by fluidic/reversed control and nonlinear structures
B2.3 - ARGO2 - Integrated design of control methods for stability of elastic aircraft
B1.9 - Validation of turbulent boundary layer-induced sound transmission through a fuselage section
B1.8 - Wind-tunnel experiments of advanced design of swept-wing with suction surfaces
B1.7 - Extension of Correlation-based Transition Transport Models for Laminar Aircraft Design
B1.6 - Effective Design Methods and Design Exploration for Laminar Wing and Fuselage
B1.5 - Sensitivities of Laminar Suction Boundary Layers for Large Reynolds Numbers
B1.3- Physics of broadband noise of sound sources from installed propulsors
JRG-B1 - Physics of Laminar Wing and Fuselage
JRG-B2 - Flow Physics of Load Reduction
B1.1 - Propeller and wing aerodynamics of distributed propulsion
B1.2 - Aerodynamic analysis of partly embedded boundary layer ingesting propulsors
B1.3 - Fast non empiric prediction of propulsion installation related noise
B1.4 - Transition Prediction and Design of Hybrid Laminar Flow Control on Blended Wing Bodies Based on 3D Parabolized Stability Equations
B2.1 - Load reduction potential of nonlinear stiffness and damping technologies
B2.2 - Structural technologies enabling load alleviation
B2.3 - Active load Reduction for enabling a 1-G wing using fOrward-looking and distributed sensors (ARGO)
B2.4 - Morphing structures for the 1g-wing
B3.1 - Global and Local Design Methodology for Laminar Flow Control
B3.2 - Process simulation and multiscale manufacturing of suction panels for laminar flow control
B3.3 - Thin Plies in Application for Next Generation Aircraft (TANGA)
B3.4 - New methods for failure and fatigue analysis of suction panels for laminar flow control
B5.1 - ADEMAO: Aircraft Design Engine based on Multidisciplinary Analysis and Optimization
JRG-B5 - Long-Range Aircraft Configurations and Technology Analyses
JRP - Permeation assessment for cryogenic applications by means of Fiber Bragg Grating sensors
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JRP - Permeation assessment for cryogenic applications by means of Fiber Bragg Grating sensors
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