Al-Kharabsheh D., Geese A., Müller R.;
changING-Ein Forschungsclub im Exzellenzcluster SE2A
Didaktik der Physik Frühjahrstagung –Bonn 2020
(2020)
Al-Kharabsheh D., Geese A., Müller R.;
Der Aufbau des Forschungsclubs changING: ingenieurdidaktisches Konzept auf Basis der Interessens- und Selbstwirksamkeit
(2022)
Beyer Y., Gücker F., Bremers E., Steen M., Hecker P.;
Incremental Passive Fault-Tolerant Control for Quadrotors With up to Three Successive Rotor Failures
CEAS
(2022)
Blech C., Hüpel Y., Langer S.;
Modelling Aspects for High-fidelity, Large-scale Aircraft Cabin Noise Simulations
Deutsche Gesellschaft für Akustik e.V. (DEGA)
(2023)
Blech C., Langer C. S.;
Wave-resolving aircraft fuselage model for cabin noise predictions under distributed fluid loadings
(2020)
Blech C., Sreekumar K. H., Römer U., Bollhöfer M., Langer C. S.;
Ein adaptives hybrides Verfahren zur Modellordnungsreduktion von dynamischen Systemen im Frequenzbereich
Deutsche Gesellschaft für Akustik e.V. (DEGA), Berlin
(2021)
Bramsiepe K., Braune M., Krüger W., Tichy L.;
Wind Tunnel Experiment with an EPP-Wing to Investigate Aeroelastic Effects of Nonlinear Elastic Stiffnesses
(2022)
Bustamante J., Hahn D., Lobitz L., Haupt M., Heimbs S.;
Enhancing Load Alleviation in Aircraft Wings through Nonlinear Behaviour
Royal Aeronautical Society
(2023)
Cao Y., Fauth L., Friebe J., Mertens A.;
Potentials to Improve the Post-Fault Performance of a Fault-Tolerant Inverter System in Electrified Aircraft Propulsion System
IEEE
(2022)
Cavaliere, Fezans u. D., Nicolas;
Recasting Discrete 1-Cosine Gust Requirements as Frequency Domain Specifications for Load Alleviation Control Design
NVvL
(2022)
Cavaliere D., Fezans N.;
A Practical Approach to Automated Multiobjective Gust Load Alleviation Control Design in a Structured H2/H-infinity Framework
CEAS
(2024)
Cavaliere D., Fezans N.;
Recasting Discrete 1-Cosine Gust Load Criteria as Frequency-domain Specifications for Load Alleviation Control Design
IFASD
(2022)
Cavaliere D., Fezans N., Kiehn D.;
Method to Account for Estimator-Induced Previewed Information Losses -- Application to Synthesis of Lidar-Based Gust Load Alleviation Functions
CEAS, Technische Universität Berlin, Germany
(2022)
Fauth L., Friebe J. a. M. P.;
Selection of Test Site Locations for LongTerm Cosmic Radiation Tests
VDE
(2021)
Fauth L., Mand P., Friebe J.;
Selection of Test Site Locations for Long-Term Cosmic Radiation Tests
Mesago PCIM GmbH
(2021)
Filippou E., Sodja J., Breuker D. R.;
Application of aeroelastic tailoring for control surface reversal
International Forum on Aeroelasticity and Structural Dynamics IFASD 2024
(2024)
Franco A., Mößner M., Ewert R., Delfs W. J.;
On the Application of Line Distributed Singularities for Fast Non-Empirical Prediction of Tonal Rotor Noise
DEGA
(2021)
Geese A., Al-Kharabsheh D., Müller R.;
MINT-Begeisterung wecken, fördern und halten - zwei Beispiele für außerschulische Lernangebote
Fachverbandes der Deutschen Physikalischen Gesellschaft
(2022)
Greco F. G., Wienke F., Bertsch L., Ring T., Langer S.;
Assessing the environmental noise of next-generation regional jet aircraft concepts in a generic airport scenario
The Acoustical Society of Korea
(2022)
Greco F. G., Wienke F., Bertsch L., Zellmann C., Schäffer B., Ring P. T., Langer C. S.;
A comparative study of semi-empirical noise emission models based on the PANAM and sonAIR aircraft noise simulation tools
Institute of Noise Control Engineering
(2022)
Gröhlich M., Böswald M., Winter R.;
An iterative eigenvalue solver for systems with frequency dependent material properties
Deutsche Gesellschaft für Akustik e.V.
(2020)
Gröhlich M., Böswald M., Winter R.;
Finite element optimization of viscoelastic damping applications
Proceedings of ISMA 2020 - International Conference on Noise and Vibration Engineering and USD 2020 - International Conference on Uncertainty in Structural Dynamics
(2020)
Gröhlich M., Böswald M., Winter R.;
Frequency and temperature dependent viscoelastic vibration damping capability of a novel local CLD treatment
International Institute of Noise Control Engineering (I-INCE)
(2020)
Hahn D., Haupt M., Heimbs S.;
Load alleviation capabilities of wings with nonlinear structural behavior in stationary and dynamic load cases
International Forum on Aeroelasticity and Structural Dynamics - IFASD 2022
(2022)
Helm S., Francois D., Krumbein A.;
Validation of CFD-based transition transport models to predict laminar-turbulent transition of swept transport aircraft wings.
STAB
(2023)
Herwig A., Haupt M., Brack T., Bustamante J., Heimbs S.;
Gust load alleviation in a scaled UAV demonstrator
ICAS
(2024)
Hüpel, Blech Y., Franco C., Delfs A., Kirsch a. W. J., Langer B., C. S.;
Comparison of different noise sources for the simulative cabin noise assessment of an electrically propelled regional aircraft
(2023)
Kopp T., Bösche D., Vieth P., Anspach F., Kurrat M., Meyer S.;
Prüfungen von Hybridschaltern in dem neuartigen Hochleistungs-Gleichstromprüffeld DC.lab der TU Braunschweig, Kontaktverhalten und Schalten
VDE VERLAG GMBH
(2022)
Krimmelbein N., Helm S., Krumbein A.;
Assessment and Adaptation of Transition Criteria for Non-Self-Similar Flows
(2024)
Lautsch, Ring M., Langer P. T., C. S.;
Validation of the Doc 29 best-practice prediction method of aircraft noise on the ground at a single flight level using ADS-B data
Deutsche Gesellschaft für Akustik e.V. (DEGA)
(2024)
Mosca V., Elham A.;
WING AEROSTRUCTURAL OPTIMIZATION WITH ACTIVE FLOW CONTROL AND ACTIVE LOAD ALLEVIATION
IDMEC Instituto Superior Técnico Universidade de Lisboa Portugal
(2021)
Schefer H., Hanisch L., Dietrich T., Mallwitz R., Henke M.;
Design of a High-Dynamic Test Bench for Accelerated Dielectric Lifetime Testing with Adjustable Voltage Slopes and Temperatures
IEEE
(2022)
Schefer H., Xu Z., Kopp T., Mallwitz R., Kurrat M.;
Investigation of Creepage Distances on Printed Circuit Boards for Avionic Applications
IEEE
(2022)
Schultz J., Blech C., Römer U., Langer C. S. u. B. M.;
Krylov Subspace Model Order Reduction for Aircraft Cabin Noise Investigation
Deutsche Gesellschaft für Akustik
(2020)
Seidler M., Rejas M. Z., Friedrichs J., Riemenschneider J.;
Introduction and Evaluation of an Aerostructural Coupling Approach for the Design of Shape Adaptive Compressor Blading
Curran Associates, Inc.
(2022)
Thamm K., Soldenhoff v. R., Lüdeke H., Scholz P.;
Experimentelle Untersuchung sequentieller Absaugung an einer ebenen Platte bei hohen Reynoldszahlen
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
(2024)
