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Johannes Dillinger
Johannes Dillinger
DLR - Institute of Aeroelasticity
在 dlr.de 的电子邮件经过验证
标题
引用次数
引用次数
年份
Stiffness optimization of composite wings with aeroelastic constraints
JKS Dillinger, T Klimmek, MM Abdalla, Z Gürdal
Journal of Aircraft 50 (4), 1159-1168, 2013
1462013
Static Aeroelastic Optimization of Composite Wings with Variable Stiffness Laminates
J Dillinger
Delft Technical University 1, 230, 2014
532014
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
432014
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
352019
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
342019
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
302013
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
252019
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
252017
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
24*2015
Investigations of passive wing technologies for load reduction
WR Krüger, J Dillinger, R De Breuker, K Haydn
CEAS Aeronautical Journal, 1-17, 2019
232019
Nonlinear Numerical Flight Dynamics for the Prediction of Maneuver Loads
M Ritter, J Dillinger
International Forum on Aeroelasticity and Structural Dynamics, No. IFASD …, 2011
202011
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
162018
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
162017
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
152016
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
142019
Design and Optimization of an Aeroservoelastic Wind Tunnel Model
JKS Dillinger, YM Meddaikar, J Lübker, M Pusch, T Kier
Fluids 5 (1), 35, 2020
132020
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
112020
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
112020
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
112016
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
102021
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