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  • ICA B "Flight Physics and Vehicle Systems"
Logo Sustainable and Energy Efficient Aviation of TU Braunschweig
JRG-B2 - Flow Physics of Load Reduction
  • 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
    • ⯇ back to research

JRG-B2 - Flow Physics of Load Reduction

Junior Research Group on "Flow Physics of Load Reduction"

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The Junior Research Group on "Flow Physics of Load Reduction" (JRG-B2) investigates and develops active load control techniques to alleviate dynamic loads on transport aircraft wings caused by gusts and unsteady flight maneuvers. The research involves numerical studies based on (U)RANS simulations, wind tunnel experiments, as well as reduced order modelling. The group was established in 2019 and currently consists of three researchers.

Active Load Reduction

Load Alleviation Principle

Aircraft wings are subject to dynamic loads caused by unsteady gusts and flight maneuvers, which reduce passenger comfort and induce structural wing deformations that are typically countered by sturdier and, consequently, heavier wing designs. To reduce the wing weight, gust and maneuver load alleviation systems are already in use in today's aircraft, where they dynamically actuate existing control surfaces like ailerons or elevators to alter the wing lift distribution during an unsteady load encounter. These systems, however, suffer from the relatively slow response of conventional control surfaces and therefore cannot exploit the full potential of gust and maneuver load alleviation.

Project Details

Scientific Staff

Dr.-Ing. André Bauknecht (Work Group Leader)

Salvatore Asaro, M.Sc. (PhD Researcher)

Khalid Khalil, M.Sc. (PhD Researcher)

Publications

A current list of publications can be found on the work group page on the website of the Institute of Fluid Mechanics (ISM).

Further information about the project

Detailed information about the research project can be found on the work group page on the website of the Institute of Fluid Mechanics (ISM).

Contact

Project lead

Dr.-Ing. André Bauknecht

Institute of Fluid Mechanics (ISM)
+49 531-391-94278

Organisation

Institute of Fluid Mechanics (ISM)

TU Braunschweig
Hermann-Blenk-Str. 37
38108 Brunswick, Germany

 

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Contact information

Cluster of Excellence SE²A –
Sustainable and Energy-Efficient Aviation
Technische Universität Braunschweig
Hermann-Blenk-Str. 42
38108 Braunschweig

se2a(at)tu-braunschweig.de
+49 531 391 66661

 

 

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