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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
B5.1 - ADEMAO: Aircraft Design Engine based on Multidisciplinary Analysis and Optimization
  • 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

B5.1 - ADEMAO: Aircraft Design Engine based on Multidisciplinary Analysis and Optimization

General Objective of the Research Project

 Referenzflugzeugkonfiguration

The research project B5.1 deals with the aircraft design development of advanced multi-fidelity aircraft design tools. In the scope of SE2A, the goal of the group is to develop an Aircraft Design Engine based on Multi-Disciplinary Analysis and Optimization (ADEMO) that uses a multi-fidelity approach in aircraft design and capable to work with unconventional aircraft configurations and advanced airframe and engine technologies. In addition, the Multi-Disciplinary Optimization (MDO) framework will be integrated to perform MDO studies of aircraft configurations.

ADEMO will be used to design a family of transport aircraft that cover the majority of air transportation needs of the future and feature all advanced technologies developed and studied within the SE2A cluster.  

ADEMO - Aircraft Design Engine based on Multi-Disciplinary Analysis and Optimization

 Allgemeine Struktur von ADEMO

ADEMO consists of multiple layers. The first layer is a full aircraft conceptual design tool, including all the relevant disciplines in aircraft design, however with a lower/medium level of fidelity. This tool is used for full aircraft conceptual design and provides general outputs such as aircraft geometry, weight breakdown, energy consumption, and mission analysis. The second layer is a surrogate modeling toolbox, which is used for connecting the results of higher fidelity and experimental analysis to the low fidelity design tool. This toolbox is also used for multi-fidelity optimization. The third layer, is a physics-based coupled-adjoint multidisciplinary design optimization (MDO) toolbox, with a medium level of fidelity. This toolbox is used for more detailed design refinements of aircraft and providing outputs, such as aircraft loads for detailed structural design. Eventually, the fourth layer is a high fidelity MDO toolbox for design optimization of selected dominant aircraft components with advanced technologies being analyzed with the Research Cluster

Details of the project

Scientific Staff

Stanislav Karpuk

Institute of Aircraft Design and Lightweight Structures

 

Publications

Y. Liu, S. Karpuk, A. Elham, “Multi-fidelity Design Optimization of a Long-range Blended Wing Body Aircraft with New Airframe Technologies”, AIAA SciTech, Orlando, FL, 6-10 January 2020.

N. Kleemann, S. Karpuk, “Conceptual Design and Optimization of a Solar-Electric Blended Wing Body Aircraft for General Aviation”, AIAA SciTech, Orlando, FL, 6- 10 January 2020.

Contact

Project Lead

Prof. Dr.-Ing. A. Elham

Institute of Aircraft Design and Lightweight Structures

Tel: +49 531 391 9930

 

 

Organisation

Technische Universität Braunschweig,
Hermann-Blenk-Straße 35, 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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