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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"
Logo Sustainable and Energy Efficient Aviation of TU Braunschweig
JRG-B5 - Long-Range Aircraft Configurations and Technology Analyses
  • 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-B5 - Long-Range Aircraft Configurations and Technology Analyses

Main Research Focus Areas

The focus of the Junior Research Group is realted to several fundamental design research questions of future sustainable aircraft design:

1. Assessement of airframe and propulsion  technologies investigated under the Se2A Cluster for the next-generation long-range commercial aircraft from the synergistic perspective. 

2. Development of methodologies for medium- and high-fidelity analyses and optimization of aircraft at the conceptual design level featuring advanced technology modeling and their integartion into the overall aircraft design process.

Design of future more sustainable long-range aircraft

Se2A LR

Potential availability of novel technologies and their effect on the overall performance of the aircraft may allow design of more unconventional aircraft configurations to further improve the overall aircraft efficiency. Moreover, performance of airframe and propulsion technologies may also limit the level of design flexibility of future aviation. Therefore, the group is focused on conceptual design of various aircraft configurations that feature potential future technologies and attempts to quantify their influence on the overall design space and capabilities of future aircraft configurations. 

Development of a multi-fidelity design framework for better technology assessments

SUAVE design environment

To perform necessary design tasks and better understand technology capabilities, performance of unconventional configurations, and uncertainties related to particular design decisions, a comprehensive multi-fidelity framework is required. The framework being developed in the Junior Research Group couples a wide variety of methods and tools from low-, medium-, and high-fidelity domanis to ensure that each capability can be used at a given conceptual design step and satisfies desired analysis or optimization goals. Moreover, the group is actively working on implimentation of novel technology estimations by means of methods integration, utimization of surrogate models, or extension of existing models to attempt to mimic desired technology behavior.

Contact

Project members

Dr.-Ing. Stanislav Karpuk

Project lead
+49 531 391 9929
s.karpuk(at)tu-braunschweig.de


M.Sc. Valerio Mosca

Research Scientist
v.mosca(at)tu-braunschweig.de  


M.Sc. Febriyan Prayoga

Research Scientist
febriyan.prayoga(at)tu-braunschweig.de

Organization

Institute of Aircraft Design and Lightweight Structures

Technical University Braunschweig
Hermann-Blenk-Straße 35 
D-38108 Braunschweig

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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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