| Author |
Manuscripts |
TAEHYOUN KIM
University of Washington Bothell, USA
|
232 Prediction of Limit Cycle Oscillations Based on Dynamic Eigen Decomposition of Flight Test Data
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Christoph Kaiser
DLR, Institute of Aeroelasticity
|
112 A general solver for the prediction of flutter and buffet onset
54 Effect of Turbulent Wedges on the Steady and Unsteady Aerodynamics of a Forward Swept Laminar Wing
123 Analysis of Linearized Motion- and Gust-Induced Airloads with a Next-Generation Computational Fluid Dynamics Solver
|
Seung-Hoon Kang
Seoul National University
|
135 Machine learning-based parametric model order reduction for the gust load analysis
|
Mordechay Karpel
Karpel Dynamic Consulting Ltd.
|
170 Aeroelastic challenges in the clean aviation hybrid-electric regional aircraft project
|
Marlus Kerninski
Embraer
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159 Wind tunnel flutter test results comparison with computational results of a half-span wing
|
Thiemo M. Kier
German Aerospace Center (DLR), Institute of System Dynamics and Control
|
107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
|
Thiemo Kier
|
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
141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test
190 Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: Case of the flipased P-Flex UAV
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
|
Spyridon Kilimtzidis
University of Patras
|
199 Application of the unsteady compressible source and doublet panel method to flutter calculations
|
Thomas Klimmek
German Aerospace Center (DLR)
|
90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
|
Johannes Knebusch
DLR German Aerospace Center
|
215 Improvement of Helicopter Fuselage Modelling - Effects of subcomponents on the overall dynamic behavior
49 Research shake test on an Airbus helicopter technology demonstrator
|
Christopher Koch
German Aerospace Center (DLR), Institute of Aeroelasticity
|
50 Influence of blade elasticity and thrust on the whirl flutter stability of a propeller-driven aircraft
18 Whirl flutter analysis using linearized propeller transfer matrices
|
Martin Kolar
Czech Aerospace Research Centre (VZLU)
|
56 New Design of Whirl Flutter Aeroelastic Demonstrator
|
Raymond Kolonay
United States Air Force Research Laboratory
|
12 Including Gradient-based Transient Gust Optimization in ASTROS
|
Ramesh Konatala
|
103 Aeroservoelastic models for design, testing, flight test clearance and validation of active flutter suppression control laws
128 Post-flight system identification and aeroservoelastic model updating for prediction and validation of the onset of flutter
|
Vassilis Kostopoulos
University of Patras
|
199 Application of the unsteady compressible source and doublet panel method to flutter calculations
|
Wolf R. Krueger
DLR Institute of Aeroelasticity
|
7 Assessment of aeroelastic stability of high aspect wing aircraft during the preliminary design
141 Assessment of Active Load Control Approaches for Transport Aircraft – Simulation and Wind Tunnel Test
|
Eduardo Krupa
Embraer
|
159 Wind tunnel flutter test results comparison with computational results of a half-span wing
|
Wolf R. Krüger
German Aerospace Center (DLR) - Institute of Aeroelasticity
|
121 Design, manufacturing and identification of an active controlled flexible wing for subsonic wind tunnel testing
58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB
|
Wolf Krüger
|
142 Nonlinear dynamic response of a pazy wing variant using Koiter-Newton model reduction
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