IFASD 2026

IFASD 2026

POSTERPRESENTATIONS

16 - 18 June 2026 | 13:00 - 14:15 CEST

ALTE MENSA - v.Trott Hall

INFORMATION FOR POSTER PRESENTATIONS

The maximum poster size is DIN A0 in portrait format.
On the first day of the forum, please hang your poster in the designated location (marked with the ID) in Room "ALTE MENSA - v.Trott Hall" before the start of the forum.
There is NO need to have any fasteners on hand.
During the lunch breaks there will be the poster discussions. Please be at your poster to discuss the topics that will be presented there.
At the end of the forum, the posters can be taken down.

IFASD2026_0307
COMBINED MECHANISM FOR MORPHING AND AEROELASTIC CONTROL
MICHAEL VALASEK, CZECH TECHNICAL UNIVERSITY, CZECH REPUBLIC
IFASD2026_0318
DYNAMIC STABILITY OF SMART WING WITH MORPHING-INDUCED CYCLIC STIFFNESS VARIATION
MANOJ PRABHAKAR, T MADRAS, CHENNAI, INDIA

IFASD2026_0099
AEROELASTIC ANALYSIS AND OPTIMIZATION OF WING DESIGN PARAMETERS AND VAT FIBER PATHS BASED ON ISOGEOMETRIC ANALYSIS
CHENG CHEN, BEIHANG UNIVERSITY, BEIJING, CHINA
IFASD2026_0102
STATE-SPACE AEROELASTIC FLUTTER ANALYSIS OF A FIXED-WING EVTOL AIRCRAFT WITH ROBUST MODAL TRACKING AND CONTINUATION
MÜSLÜM ÖZKESICILER, ASELSAN A.S., ANKARA, TURKEY
IFASD2026_0136
AEROELASTICITY STUDY OF MULTI-BODY COMBINED UNMANNED AERIAL VEHICLES
GUIXI HUO, BEIHANG UNIVERSITY, BEIJING, CHINA

IFASD2026_0298
NUMERICAL INVESTIGATION OF STRESS REDISTRIBUTION IN AIRCRAFT ENGINE PYLON USING GEOMETRY-BASED STRUCTURAL OPTIMIZATION
JAVAD RASHID JAFARI, ALPARSALAN UNIVERSITY, ADANA, TURKEY

IFASD2026_0268
GUST LOAD ANALYSIS OF AIRCRAFT WINGS WITH DISTRIBUTED ROTORS
NICOLAS MAXIMILIAN LEONARD GARRIDO, UNIVERSITY OF NOTTINGHAM, NOTTINGHAM, UNITED KINGDOM

IFASD2026_0126
A CO-KRIGING-BASED FLUTTER BOUNDARY PREDICTION METHOD INTEGRATING AEROELASTIC MODELS WITH FLIGHT TEST DATA
PENGHUI CHAO, BEIHANG UNIVERSITY, BEIJING, CHINA

IFASD2026_0206
ANALYSIS OF NONLINEAR DYNAMIC CHARACTERISTICS OF LARGE FLEXIBLE WINGS BASED ON STRUCTURAL REDUCED ORDER MODEL
RUI ZHAO, SCHOOL OF AERONAUTIC SCIENCE AND ENGINEERING, BEIHANG UNIVERSITY, BEIJING, CHINA
IFASD2026_0271
A POD-BASED STRUCTURAL-PARAMETRIC AERODYNAMIC REDUCED-ORDER MODEL: VALIDATION ON AGARD 445.6 WING
CHANG MA, NORTHWESTERN POLYTECHNICAL UNIVERSITY, XI'AN, CHINA