Stiffness optimization of composite wings with aeroelastic constraints JKS Dillinger, T Klimmek, MM Abdalla, Z Gürdal Journal of Aircraft 50 (4), 1159-1168, 2013 | 155 | 2013 |
Static Aeroelastic Optimization of Composite Wings with Variable Stiffness Laminates J Dillinger Delft Technical University 1, 230, 2014 | 54 | 2014 |
Computational aeroelastic investigation of a transonic limit-cycle-oscillation experiment at a transport aircraft wing model B Stickan, J Dillinger, G Schewe Journal of Fluids and Structures 49, 223-241, 2014 | 44 | 2014 |
Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings C Roessler, P Stahl, F Sendner, A Hermanutz, S Koeberle, ... AIAA Scitech 2019 Forum, 1813, 2019 | 39 | 2019 |
Aircraft Aeroservoelastic Modelling of the FLEXOP Unmanned Flying Demonstrator YM Meddaikar, J Dillinger, T Klimmek, W Krueger, M Wuestenhagen, ... AIAA Scitech 2019 Forum, 1815, 2019 | 39 | 2019 |
Static aeroelastic stiffness optimization and investigation of forward swept composite wings J Dillinger, MM Abdalla, T Klimmek, Z Gürdal 10th World Congress on Structural and Multidisciplinary Optimization, 19-24, 2013 | 31 | 2013 |
Aeroelastic Modeling and Control of an Experimental Flexible Wing M Pusch, D Ossmann, J Dillinger, TM Kier, M Tang, J Lübker AIAA Scitech 2019 Forum, 0131, 2019 | 26 | 2019 |
Static and Dynamic Aeroelastic Validation of a Flexible Forward Swept Composite Wing M Ritter, J Dillinger, YM Meddaikar 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017 | 25 | 2017 |
Static Aeroelastic Stiffness Optimization of a Forward Swept Composite Wing with CFD Corrected Aero Loads J Dillinger, MM Abdalla, YM Meddaikar, T Klimmek Proc. International Forum on Aeroelasticity and Structural Dynamics, IFASD 28, 2015 | 25* | 2015 |
Investigations of passive wing technologies for load reduction WR Krüger, J Dillinger, R De Breuker, K Haydn CEAS Aeronautical Journal, 1-17, 2019 | 24 | 2019 |
Tailoring of a Composite Regional Jet Wing Using the Slice and Swap Method GHC Silva, AP do Prado, PH Cabral, R De Breuker, JKS Dillinger Journal of Aircraft, 1-15, 2018 | 24 | 2018 |
Nonlinear Numerical Flight Dynamics for the Prediction of Maneuver Loads M Ritter, J Dillinger International Forum on Aeroelasticity and Structural Dynamics, No. IFASD …, 2011 | 20 | 2011 |
Optimization & Testing of Aeroelastically-Tailored Forward Swept Wings MY Meddaikar, J Dillinger, MR Ritter, Y Govers IFASD 2017-International Forum on Aeroelasticity and Structural Dynamics, 1-13, 2017 | 16 | 2017 |
Ground Testing of the FLEXOP Demonstrator Aircraft J Sodja, R De Breuker, YM Meddaikar, JK Dillinger, K Soal, Y Govers, ... AIAA Scitech 2020 Forum, 1968, 2020 | 15 | 2020 |
Design and wind tunnel test of an actively controlled flexible wing WR Krüger, J Dillinger, MY Meddaikar, J Lübker, M Tang, T Meier, ... Proc. International Forum on Aeroelasticity and Strucutural Dynamics 2019, 2019 | 15 | 2019 |
Optimization, Manufacturing and Testing of a Composite Wing with Maximized Tip Deflection YM Meddaikar, JK Dillinger, J Sodja, H Mai, R De Breuker 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016 | 15 | 2016 |
Design and Optimization of an Aeroservoelastic Wind Tunnel Model JKS Dillinger, YM Meddaikar, J Lübker, M Pusch, T Kier Fluids 5 (1), 35, 2020 | 14 | 2020 |
Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft C Roessler, J Bartasevicius, SJ Koeberle, D Teubl, M Hornung, ... AIAA Scitech 2020 Forum, 1969, 2020 | 14 | 2020 |
Dynamic Response of Aeroelastically Tailored Composite Wing: Analysis and Experiment J Sodja, N Werter, J Dillinger, R De Breuker 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016 | 11 | 2016 |
Measurements of deformation, schlieren and forces on an OAT15A airfoil at pre-buffet and buffet conditions A Accorinti, T Baur, S Scharnowski, J Knebusch, J Dillinger, Y Govers, ... IOP Conference Series: Materials Science and Engineering 1024 (1), 012052, 2021 | 10 | 2021 |