Authors Index

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Author	Manuscripts
Hamed Haddad Khodaparast	14 Gust load alleviation efficiency in an optimized composite wing through the integration of wingtip devices: Incorporating folding and twist strategies 15 Optimizing high aspect ratio composite wings through geometrically nonlinear aeroelastic tailoring 33 Aeroelastic hybrid testing for industrial applications
Michael Hadjipantelis University of Bath	26 Preliminary investigation of the superelastic monostable spoiler for dynamic gust loads alleviation
Zhang Haibo	136 The Design and Analysis of Tensegrity Morphing Wing
Vega Handojo DLR German Aerospace Center	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft 4 Influence of Cruise Altitude Variation on the Turbulence Loads of a Medium-Range Transport Configuration
Charlotte Hanke German Aerospace Center (DLR), Institute of Aeroelasticity	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings 202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil 106 Design and Experimental Characterization of a Gust-Generator Concept with Rotating-Slotted Cylinders in the Low-Speed Wind Tunnel DNW-NWB 107 Wind Tunnel Testing Active Gust Load Alleviation of a Flexible Wing
Patrick Hartl	202 Experimental investigation of shock control bumbs on the transonic dip of the OAT15A airfoil
Oleh Havaza National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”	235 Mathematical method for prediction aeroelastic phenomena and multidisciplinary optimization lifting surfaces of flight vehicle at preliminary stage design
Longfei He	63 A CFD/CTD/CSD based aero-thermo-elastic framework for full-vehicle scale analysis
Fintan Healy University of Bristol	125 Active flutter suppression and gust load alleviation of wings incorporating floating wingtips 122 Wing mounted hydrogen fuel tanks: mitigating the aeroelastic penalties of dry wing configurations?
Tobias Hecken German Aerospace Center (DLR)	90 The Effect of Aspect Ratio Variation on the Preliminary Aeroelastic Assessment of a Mid-Range Transport Aircraft
Benjamin Herrmann Hamburg University of Technology	46 Doublet lattice modelling and analysis of unsteady aerodynamic effects for a flexible unmanned aircraft during maneuvers and gust encounters
Pedro Higino Cabral Embraer S. A.	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Jonathan Hilger DLR	58 Wind tunnel testing and modal validation of TU-Flex's high aspect-ratio wings
Mirko Hornung Technical University of Munich	24 Experimental and numerical assessment on the aeroelastic behavior of a NLF airfoil with oscillating control surfaces 10 Wing shape control on the D150 model with aspect ratio tradeoffs for fuel efficiency improvement 116 Lessons Learned from Flight Testing Active Flutter Suppression Technologies
Vladimír Hostinský Brno University of Technology - FME - Institute of Aerospace Engineering	133 Unified model of sandwich panel core and faces for aeroelastic optimization
Yingyou Hou	240 Aeroelastic characteristics of plane-symmetry vehicle main wing trailing edge rudder at high angle of attack
Kunhui Huang	11 Wind tunnel test of gust response for distributed propeller-wing system 156 Measurement and Control System Design for Propeller-Wing System Experiments

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]