Authors Index

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Author	Manuscripts
Hoang Thien Phu VO	88 Aircraft vibration from React to Predict
Bálint Vanek	196 Co-Design of the Aeroelastic Wing Parameters and the Flutter Control Law 99 Flexible aircraft conceptual co-design based on the RCE framework 128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
Balint Vanek SZTAKI	116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies 103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Santosh Varigonda North Carolina State University	81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow
Srikanth Vasudevan Delft University of Technology	164 Mechanism of transonic aeroelastic instabilities via synchronization of coupled oscillators
Kartik Venkatraman Indian Institute of Science	176 Transonic shock oscillations in an oscillating finite span wing 175 Prediction of transonic buffet in an axial flow fan using global stability analysis
Fabio Vetrano Airbus Operations SAS	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device
Silvia Vettori Siemens Digital Industry Software NV	225 Experimental And Numerical Activities For Aeroelastic Analysis Of An Aluminum Wing
Ondrej Vich Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Cyrille Vidy Airbus Defence & Space GmbH	47 From Multivariate Random Loads To Deterministic Load Distributions: An Exact Method For Aeroelastic Design 44 Robust design through identification of main components from multivariate random loads
Coen de Visser Delft University of Technology	198 Flexible aircraft flight dynamics and loads model identification from flight test data in unsteady conditions
Alessandra Vizzaccaro	33 Aeroelastic hybrid testing for industrial applications
Jarmil Vlach Czech Aerospace Research Centre (VZLU)	56 New Design of Whirl Flutter Aeroelastic Demonstrator
Robin Volkmar DLR	113 Reliable monitoring of modal parameters during a flight vibration test using autonomous modal analysis and a Kalman filter 119 Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns 190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
Arne Voß DLR	1 Gust Encounter of a Supersonic Fighter Aircraft using CFD Methods 58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Pierre Vuillemin DTIS, ONERA, Universite de Toulouse, 31000, Toulouse, France	227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration

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