Yves Govers

发表

Solar Impulse - Ground vibration testing and finite element model validation of a lightweight aircraft

Marc Böswald, Arne Vollan, Yves Govers, 2011 .

Design of a Rotor Blade Tip for the Investigation of Dynamic Stall in the Transonic Wind Tunnel Göttingen

Yves Govers, Benjamin Lütke, Johannes Nuhn, 2016 .

Identification of Modal Parameters of Aircraft during Taxi

Marc Böswald, Dennis Göge, Yves Govers, 2008 .

AIRBUS A350 XWB GVT: State-of-the-Art Techniques to Perform a Faster and Better GVT Campaign

Yves Govers, Pascal Lubrina, Stéphane Giclais, 2014 .

The use of strain sensors for modal identification of aeroelastic structures

Yves Govers, G. Jelicic, Taner Akbay, 2016 .

VALIDATING GLOBAL STRUCTURAL DAMPING MODELS FOR DYNAMIC ANALYSES

Marc Böswald, Yves Govers, Martin Höser, 2015 .

STATE-OF-THE-ART TECHNIQUES TO PERFORM AN INDUSTRIAL VIBRATION TEST CAMPAIGN AND A RAPID PROCESS TO UPDATE RENEWED FEM FOR CLEARANCE OF FIRST FLIGHT TEST

Marc Böswald, Yves Govers, Pascal Lubrina, 2015 .

New Concepts for Ground and Flight Vibration Testing of Aircraft based on Output-Only Modal Analysis

Marc Böswald, Yves Govers, G. Jelicic, 2017 .

Fast Online Monitoring and System Identification for the Application in the Field of Aeroelasticity

Marc Böswald, Yves Govers, G. Jelicic, 2015 .

Real-time assessment of flutter stability based on automated output-only modal analysis

Marc Böswald, Yves Govers, G. Jelicic, 2014 .

Model updating strategy of the DLR-AIRMOD test structure

Edoardo Patelli, John E. Mottershead, Matteo Broggi, 2017 .

The Sensitivity Method in Stochastic Model Updating

John E. Mottershead, Hamed Haddad Khodaparast, Yves Govers, 2015 .

Model validation of an aeroelastically-tailored forward swept wing using fibre-optical strain measurements

Yves Govers, Muhammad Yasser Meddaikar, Kautuk Sinha, 2018 .

System identification and tracking using a statistical model and a Kalman filter

Anriëtte Bekker, Yves Govers, Jörg Bienert, 2019, Mechanical Systems and Signal Processing.

A Review of Experimental Modal Analysis Methods with respect to their Applicability to Test Data of Large Aircraft Structures

Marc Böswald, Dennis Göge, Yves Govers, 2006 .

Vibro-acoustic analysis of flight test data comprising fuselage vibrations, external pressure and interior cabin noise measurements

Marc Böswald, Yves Govers, Marco Norambuena, 2016 .

Inverse quantification of epistemic uncertainty under scarce data: Bayesian or Interval approach?

Edoardo Patelli, John E. Mottershead, David Moens, 2019 .

Efficient ground vibration testing of aircraft based onoutput-only modal analysis during taxi

Marc Böswald, Ralf Buchbach, Yves Govers, 2017 .

Optimization & Testing of Aeroelastically-Tailored Forward Swept Wings

Yves Govers, Johannes Dillinger, Muhammad Yasser Meddaikar, 2017 .

Analysis of Sources and Quantification of Uncertainty in Experimental Modal Data

Marc Böswald, Dennis Göge, Michael Link, 2006 .

A multivariate interval approach for inverse uncertainty quantification with limited experimental data

Edoardo Patelli, Michael Beer, John E. Mottershead, 2019, Mechanical Systems and Signal Processing.

Solar Impulse – How to validate the numerical model of asuperlight aircraft with A340 dimensions!

Marc Böswald, A. Vollan, Yves Govers, 2010 .

Recent developments in operational modal analysis for ground and flight vibration testing

Marc Böswald, Yves Govers, G. Jelicic, 2017 .

Interval model updating of the AIRMOD structure

John E. Mottershead, Michael Link, Hamed Haddad Khodaparast, 2012 .

Measurement of FRFs and modal identification in case of correlated multi-point excitation

U. Fuellekrug, Yves Govers, M. Boeswald, 2008 .

Advanced systems and services for ground vibration testing - Application for a research test on an Airbus A340-600 aircraft

Marc Böswald, Bart Peeters, Jan Debille, 2011 .

An extensive helicopter Ground Vibration Test: from pretest analysis to the study of non-linearities

Marc Böswald, Yves Govers, Martijn Priems, 2018 .

Using stochastic experimental modal data for identifying stochastic finite element parameters of the AIRMOD benchmark structure

Michael Link, Yves Govers, 2012 .

Latest design trends in modal accelerometers for aircraft ground vibration testing

Thomas Petzsche, Yves Govers, Julian Sinske, 2020 .

Taxi Vibration Testing - An Alternative Method to Ground Vibration Testing of Large Aircraft

Marc Böswald, Yves Govers, 2008 .

Perspectives on model updating

Edoardo Patelli, John E. Mottershead, Herbert Martins Gomes, 2015 .

Ground Vibration Test of the COSDYNA Wind Tunnel Model

Marc Böswald, Yves Govers, 2006 .

Quantification and Error Source Classification of Uncertainty in Experimental Modal Data Supported by Stochastic Finite Element Analysis

Marc Böswald, Dennis Göge, Yves Govers, 2007 .

AIRBUS A350XWB Ground Vibration Testing: Efficient techniques for customer oriented on-site modal identification

Marc Böswald, Yves Govers, Pascal Lubrina, 2014 .

Preparation and execution of the NICETRIP low- and high-speed wind tunnel tests

Oliver Schneider, Yves Govers, A. Ragazzi, 2016 .

Stochastic Model Updating of the DLR AIRMOD Structure

John E. Mottershead, Michael Link, Hamed Haddad Khodaparast, 2014 .

Online Monitoring of Aircraft Modal Parameters during Flight Test based on permanent Output-only Modal Analysis

Ralf Buchbach, Yves Govers, G. Jelicic, 2017 .

Parameter identification of structural dynamic models by inverse statistical analysis

Yves Govers, Y. Govers, 2012 .

Ground Testing of the FLEXOP Demonstrator Aircraft

Bálint Vanek, Panagiotis Georgopoulos, Christos Koimtzoglou, 2020, AIAA Scitech 2020 Forum.

Flight testing using fast online aeroelastic identification techniques with DLR research aircraft HALO

Marc Böswald, Ralf Buchbach, Yves Govers, 2017 .

Comparison between Bayesian and intervaluncertainty quantification: application to theAIRMOD test structure

Edoardo Patelli, David Moens, Michael Beer, 2017 .

A SYSTEMATIC INVESTIGATION OF COMMON GRADIENT BASED MODEL UPDATING APPROACHES APPLIED TO HIGH-FIDELITY TEST-DATA OF A WIND TURBINE ROTOR BLADE

Yves Govers, Johannes Knebusch, Janto Gundlach, 2020 .

NEW EXCITATION SIGNALS FOR AIRCRAFT GROUND VIBRATION TESTING

Marc Böswald, Yves Govers, Pascal Lubrina, 2011 .

Identification and assessment of a nonlinear dynamic actuator model for controlling an experimental flexible wing

Marc Böswald, Martin Tang, Manuel Pusch, 2021, CEAS Aeronautical Journal.

Sensitivity or Bayesian model updating: a comparison of techniques using the DLR AIRMOD test data

Edoardo Patelli, John E. Mottershead, Michael Link, 2017 .

Model updating using uncertain experimental modal data

Michael Link, Yves Govers, Y. Govers, 2011 .

A comparison of two stochastic model updating methods using the DLR AIRMOD test structure

John E. Mottershead, Michael Link, Hamed Haddad Khodaparast, 2015 .

Comparison of Bayesian and interval uncertainty quantification: Application to the AIRMOD test structure

Edoardo Patelli, David Moens, Matteo Broggi, 2017, 2017 IEEE Symposium Series on Computational Intelligence (SSCI).

Fuzzy model updating and its application to the DLR Airmod structure

John E. Mottershead, Michael Link, Johann Sienz, 2014 .

Stochastic model updating—Covariance matrix adjustment from uncertain experimental modal data

Michael Link, Yves Govers, Y. Govers, 2010 .