A review on non-linear aeroelasticity of high aspect-ratio wings
Current economic constraints and environmental regulations call for design of more efficient
aircraft configurations. An observed trend in aircraft design to reduce the lift induced drag …
aircraft configurations. An observed trend in aircraft design to reduce the lift induced drag …
An efficient two-step damage identification method using sunflower optimization algorithm and mode shape curvature (MSDBI–SFO)
GF Gomes, RS Giovani - Engineering with Computers, 2022 - Springer
Laminated composite structures performance and behavior can be affected by damage that
is not always visible on the surface. The need to monitor the health of these structures has …
is not always visible on the surface. The need to monitor the health of these structures has …
Aircraft loss of control problem analysis and research toward a holistic solution
CM Belcastro, JV Foster, GH Shah… - Journal of Guidance …, 2017 - arc.aiaa.org
AIRCRAFT loss of control (LOC) remains one of the largest contributors to fatal accidents. As
shown in Fig. 1, in-flight loss of control was the largest fatal accident category for large …
shown in Fig. 1, in-flight loss of control was the largest fatal accident category for large …
Probabilistic learning for modeling and quantifying model‐form uncertainties in nonlinear computational mechanics
Recently, a novel nonparametric probabilistic method for modeling and quantifying model‐
form uncertainties in nonlinear computational mechanics was proposed. Its potential was …
form uncertainties in nonlinear computational mechanics was proposed. Its potential was …
[PDF][PDF] Comprehensive simulation of a complete tiltrotor with pilot-in-the-loop for whirl-flutter stability analysis
This work presents the complete aero-servo-elastic model Bell XV-15 tilt-rotor equipped with
Advanced Technology Blades (ATB). Multibody and aerodynamic modeling of each …
Advanced Technology Blades (ATB). Multibody and aerodynamic modeling of each …
maewing2: conceptual design and system test
CD Regan - AIAA Atmospheric Flight Mechanics Conference, 2017 - arc.aiaa.org
The conceptual design, build plan, and test plan of a flexible, flying wing aircraft, the
mAEWing2, has been accomplished. mAEWing2 is a 50% scaled aircraft based on the X …
mAEWing2, has been accomplished. mAEWing2 is a 50% scaled aircraft based on the X …
Modeling and quantification of model-form uncertainties in eigenvalue computations using a stochastic reduced model
A feasible, nonparametric, probabilistic approach for modeling and quantifying model-form
uncertainties associated with a computational model designed for the solution of a …
uncertainties associated with a computational model designed for the solution of a …
Optimal sabotage attack on composite material parts
Industry 4.0 envisions a fully automated manufacturing environment, in which computerized
manufacturing equipment—Cyber-Physical Systems (CPS)—performs all tasks. These …
manufacturing equipment—Cyber-Physical Systems (CPS)—performs all tasks. These …
An overview of methods for investigation of aeroelastic response on high aspect ratio fixed-winged aircraft
The thrust of increasing environmental and economic constraints on aircraft has enthused
accelerated research in design of more economical and higher performance aircraft …
accelerated research in design of more economical and higher performance aircraft …
Development of a low-cost flutter test bed with an EPS foam model for preliminary wing design
This paper discusses a novel, low-cost approach for the design and testing of a flutter test
article made out of expanded polystyrene (EPS) foam. The low mass of this test article …
article made out of expanded polystyrene (EPS) foam. The low mass of this test article …