SFB-TRR 364 Synergies of Highly Integrated Transport Aircraft

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1 to 10 of 20 Results

SynTrac_A03(DLR) Oct 29, 2026 Aerodynamic coupling of propulsion, airframe, and control surfaces for aircraft with distributed and integrated propulsion systems
SynTrac_A06(TU Braunschweig / Universität Stuttgart / LU Hannover) Oct 27, 2026 Conceptual design asessment and optimization of highly integrated transport aircraft
Replication Data for: "Laser-Induced Phosphor Thermography on Surfaces in Humid Crossflow using Zinc Oxide" Oct 26, 2026 - SynTrac_C02 Fuhrmann, Tobias; Lamanna, Grazia, 2026, "Replication Data for: "Laser-Induced Phosphor Thermography on Surfaces in Humid Crossflow using Zinc Oxide"", https://doi.org/10.18419/DARUS-6572, DaRUS, V1 The increase of water content of the exhaust gas due to direct injection of water into the combustion chamber or the addition of urea to the exhaust gas promotes contrail formation and makes the water recovery in turbomachinery a potential benefit. In this work, Laser-Induced Phosphor Thermography (LIPT) based on the spectral intensity ratio method...
SynTrac_B02(Universität Stuttgart) Oct 20, 2026 Exploitation of Aerodynamic-Airframe Interaction by Integrated Design
Exergy-Anergy Based Off-Design Performance Model of Turbofan Core Engine Oct 20, 2026 - SynTrac_B04 Varchev, Tihomir; Yuan, Yiwen; Schateikis, Tobias; Staudacher, Stephan, 2026, "Exergy-Anergy Based Off-Design Performance Model of Turbofan Core Engine", https://doi.org/10.18419/DARUS-6532, DaRUS, V1, UNF:6:8Lhxf2Yo13emb2DsJtVymQ== [fileUNF] Exergy-Anergy based performance maps of turbomachinery components provide a consistent and physically interpretable representation of their whole operating range. This dataset comprises two exergy-anergy performance maps - one of a high-pressure compressor and one of a high-pressure turbine. Furthermore, it contains the results of performance calcu...
Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites" Oct 15, 2026 - SynTrac_B06 Friedrichs-Dachale, Maximilian; Haupt, Matthias, 2026, "Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites"", https://doi.org/10.18419/DARUS-6535, DaRUS, V1, UNF:6:zpi9ZGPWr/sq1NUZEm1FRA== [fileUNF] Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites". The structure of the replication data can be found in the README.md.
SynTrac_B06(TU Braunschweig / Universität Stuttgart) Oct 14, 2026 Structural Design Space and Interphases of AFT-Mounted Engines - Methodology Framework, Structural Design and Optimization
Supplementary Data for: Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations Jul 10, 2026 - SynTrac_C02 Gösele, David, 2026, "Supplementary Data for: Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations", https://doi.org/10.18419/DARUS-6277, DaRUS, V1, UNF:6:jDcZj6lULVavH2bv0EkZIQ== [fileUNF] Data and Animations to the manuscript: David Gösele, Johannes C. Müller, Jonathan Wurst, Mathis Fricke, Kathrin Schulte "Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations", referred to as "related publication" in the following: We propose a boundary condition for the volume-of-fluid (VOF) method that uses...
SynTrac_C02(Universität Stuttgart) Jul 3, 2026 Exhaust gas treatment and thermal management in advanced propulsion systems by use of porous media
Data for: "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft" May 27, 2026 - SynTrac_B04 Yuan, Yiwen; Staudacher, Stephan, 2026, "Data for: "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft"", https://doi.org/10.18419/DARUS-5605, DaRUS, V1 This is the reference NPSS model used for data generation for paper "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft" presented at EASN 2025, Spain. The sensitivity study made in this paper is based on this model with corresponding modifications in each relevant engine component.

SynTrac_A03(DLR)

Oct 29, 2026

Aerodynamic coupling of propulsion, airframe, and control surfaces for aircraft with distributed and integrated propulsion systems

SynTrac_A06(TU Braunschweig / Universität Stuttgart / LU Hannover)

Oct 27, 2026

Conceptual design asessment and optimization of highly integrated transport aircraft

Replication Data for: "Laser-Induced Phosphor Thermography on Surfaces in Humid Crossflow using Zinc Oxide"

Oct 26, 2026 - SynTrac_C02

Fuhrmann, Tobias; Lamanna, Grazia, 2026, "Replication Data for: "Laser-Induced Phosphor Thermography on Surfaces in Humid Crossflow using Zinc Oxide"", https://doi.org/10.18419/DARUS-6572, DaRUS, V1

The increase of water content of the exhaust gas due to direct injection of water into the combustion chamber or the addition of urea to the exhaust gas promotes contrail formation and makes the water recovery in turbomachinery a potential benefit. In this work, Laser-Induced Phosphor Thermography (LIPT) based on the spectral intensity ratio method...

SynTrac_B02(Universität Stuttgart)

Oct 20, 2026

Exploitation of Aerodynamic-Airframe Interaction by Integrated Design

Exergy-Anergy Based Off-Design Performance Model of Turbofan Core Engine

Oct 20, 2026 - SynTrac_B04

Varchev, Tihomir; Yuan, Yiwen; Schateikis, Tobias; Staudacher, Stephan, 2026, "Exergy-Anergy Based Off-Design Performance Model of Turbofan Core Engine", https://doi.org/10.18419/DARUS-6532, DaRUS, V1, UNF:6:8Lhxf2Yo13emb2DsJtVymQ== [fileUNF]

Exergy-Anergy based performance maps of turbomachinery components provide a consistent and physically interpretable representation of their whole operating range. This dataset comprises two exergy-anergy performance maps - one of a high-pressure compressor and one of a high-pressure turbine. Furthermore, it contains the results of performance calcu...

Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites"

Oct 15, 2026 - SynTrac_B06

Friedrichs-Dachale, Maximilian; Haupt, Matthias, 2026, "Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites"", https://doi.org/10.18419/DARUS-6535, DaRUS, V1, UNF:6:zpi9ZGPWr/sq1NUZEm1FRA== [fileUNF]

Replication Data for: "A Scale-Bridging Analysis Framework for a Rear Fuselage Structure with Embedded Engines Using Isogeometric Analysis and Auxetic Sandwich Composites". The structure of the replication data can be found in the README.md.

SynTrac_B06(TU Braunschweig / Universität Stuttgart)

Oct 14, 2026

Structural Design Space and Interphases of AFT-Mounted Engines - Methodology Framework, Structural Design and Optimization

Supplementary Data for: Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations

Jul 10, 2026 - SynTrac_C02

Gösele, David, 2026, "Supplementary Data for: Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations", https://doi.org/10.18419/DARUS-6277, DaRUS, V1, UNF:6:jDcZj6lULVavH2bv0EkZIQ== [fileUNF]

Data and Animations to the manuscript: David Gösele, Johannes C. Müller, Jonathan Wurst, Mathis Fricke, Kathrin Schulte "Numerical method for imposing a pinned contact line boundary condition in 2D VOF simulations", referred to as "related publication" in the following: We propose a boundary condition for the volume-of-fluid (VOF) method that uses...

SynTrac_C02(Universität Stuttgart)

Jul 3, 2026

Exhaust gas treatment and thermal management in advanced propulsion systems by use of porous media

Data for: "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft"

May 27, 2026 - SynTrac_B04

Yuan, Yiwen; Staudacher, Stephan, 2026, "Data for: "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft"", https://doi.org/10.18419/DARUS-5605, DaRUS, V1

This is the reference NPSS model used for data generation for paper "The Challenges in Extending Engine Performance Modelling for Highly Integrated Transport Aircraft" presented at EASN 2025, Spain. The sensitivity study made in this paper is based on this model with corresponding modifications in each relevant engine component.

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