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2020 |
Crosby, Kevin M. |
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2020 |
Coppotelli, Giuliano |
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2020 |
Kamali, Soudeh |
| DEPLOYABLE WING MODEL USING ANCF AND UVLM: MULTIBODY DYNAMIC SIMULATION AND WIND TUNNEL EXPERIMENT
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2020 |
Otsuka, Keisuke |
| MULTIBODY DYNAMICS SIMULATIONS OF DISTRIBUTED ELECTRIC PROPELLERS OF X-57 AIRCRAFT
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2020 |
Nelson, Kyle J. |
| MULTIPLE SHAKER PLACEMENT FOR GROUND VIBRATION TEST OF X-59 AIRCRAFT USING TOPOLOGY OPTIMIZATION
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2020 |
Pak, Chan-gi |
| ON THE OPERATIONAL MODAL ANALYSIS TECHNIQUES FOR THE ESTIMATE OF MODAL PARAMETERS OF AIRCRAFT STRUCTURES DURING FLYING VIBRATION
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2020 |
Covioli, Jacopo Valentino |
| AEROELASTIC TESTING FOR FREEPLAY INDUCED LIMIT CYCLES OF FLEXIBLE WING-AILERON SYSEM
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2020 |
He, Xufei |
| A DATABASE OF FLUTTER CHARACTERISTICS FOR SIMPLE LOW AND MEDIUM ASPECT RATIO WINGS AT LOW SPEED
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2020 |
Fernandez, Elena De Oro |
| EXPERIMENTAL INVESTIGATION OF MISTUNING AND DAMPING CHARACTERISTICS OF A BLADED DISK AT OPERATIONAL SPEED UNDER SYNCHRONOUS VIBRATION
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2020 |
Kurstak, Eric |
| REDUCTION METHOD BASED STRUCTURAL MODEL UPDATING METHOD VIA NEURAL NETWORKS
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2020 |
Sung, Heejun |
| SLOSHING ROMS FOR FLUID-STRUCTURE INTERACTIONS IN AEROSPACE APPLICATIONS
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2020 |
Mastroddi, Franco |
| MULTI-FIDELITY DESIGN OF AN AEROELASTICALLY TAILORED COMPOSITE WING FOR DYNAMIC WIND-TUNNEL TESTING
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2020 |
Mitrotta, Francesco Mario Antonio |
| DISCRETE TIME STATE-SPACE AEROSERVOELASTIC MODELING USING FUNG3D
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2020 |
Wang, Zhicun |
| AEROSERVOELASTIC RESPONSE AND STABILITY FRAMEWORK WITH COMPUTATIONAL AERODYNAMICS
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2020 |
Karpel, Moti |
| GROUND VIBRATION TESTING ON VERY FLEXIBLE AIRCRAFT
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2020 |
Shargi, Bilal |
| INVERSE METHODS FOR IDENTIFYING PRESSURE LOADING VEHICLES USING STRUCTURAL RESPONSE
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2020 |
Coffin, Peter |
| MODELING PYROSHOCK ATTENUATION IN SPACE STRUCTURES
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2020 |
Babuska, Vit |
| ANALYZING THE DYNAMIC BEHAVIOR OF A HIGH ASPECT RATIO WING INCORPORATING A FOLDING WINGTIP
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2020 |
Cheung, Ronald C. |
| A MONTE CARLO SIMULATION METHOD FOR NON-RANDOM LIMIT CYCLE OSCILLATION
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2020 |
Lyman, Tyler |
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