Dynamic sensitivity-based finite element model updating for nonlinear structures using time-domain responses
To obtain the numerical model for predicting the nonlinear dynamic responses with high
accuracy, a dynamic sensitivity-based model updating approach by using the time-domain …
accuracy, a dynamic sensitivity-based model updating approach by using the time-domain …
Modeling, design, and flight testing of three flutter controllers for a flying-wing drone
Three flutter-suppression designs for a flexible flying-wing research drone are discussed,
along with the modeling and flight-test results. The drone, with wing span of 10 feet, aspect …
along with the modeling and flight-test results. The drone, with wing span of 10 feet, aspect …
Active flutter mitigation testing on the FLEXOP demonstrator aircraft
The paper details the research and corresponding implementation and testing steps of the
FLEXOP demonstrator aircraft. Within the EU funded project an unmanned demonstrator …
FLEXOP demonstrator aircraft. Within the EU funded project an unmanned demonstrator …
Damage and damping identification in a structure through novel damped updating method
S Sehgal, H Kumar - Iranian Journal of Science and Technology …, 2021 - Springer
In this paper, damages as well as damping effects present in a structure have been
identified through the use of a two-stage damped updating method. The structure was …
identified through the use of a two-stage damped updating method. The structure was …
Flight-dynamics and flutter analysis and control of an MDAO-designed flying-wing research drone
The flight dynamics, flutter, and control design for two flexible flying-wing research drones
are discussed. The drones, with wing spans of 10 to 14 feet, aspect ratios of over 10, and …
are discussed. The drones, with wing spans of 10 to 14 feet, aspect ratios of over 10, and …
mAEWing2: Initial Flight Test and System Identification of a Flexible UAV
CD Regan, A Kotikalpudi, DK Schmidt… - AIAA Scitech 2020 …, 2020 - arc.aiaa.org
The flight testing, system identification, and model refinement of a flexible, flying wing
aircraft, the mAEWing2, has been accomplished with an emphasis on a research-through …
aircraft, the mAEWing2, has been accomplished with an emphasis on a research-through …
Finite element model updating for very flexible wings
B Sharqi, CES Cesnik - Journal of Aircraft, 2023 - arc.aiaa.org
As aircraft wings become more flexible as a result of searching for more fuel efficient and
higher performance solutions, structural nonlinearities become more apparent. Geometric …
higher performance solutions, structural nonlinearities become more apparent. Geometric …
The development of a flight test platform to study the body freedom flutter of BWB flying wings
P Shi, F Liu, Y Gu, Z Yang - Aerospace, 2021 - mdpi.com
A flight test platform is designed to conduct an experimental study on the body freedom
flutter of a BWB flying wing, and a flight test is performed by using the proposed platform. A …
flutter of a BWB flying wing, and a flight test is performed by using the proposed platform. A …
Model updating and aeroelastic correlation of a scaled wind tunnel model for active flutter suppression test
D Di Leone, F Lo Balbo, A De Gaspari, S Ricci - Aerospace, 2021 - mdpi.com
This article presents a modal correlation and update carried out on an aeroelastic wind
tunnel demonstrator representing a conventional passenger transport aircraft. The aim of …
tunnel demonstrator representing a conventional passenger transport aircraft. The aim of …
Flight Dynamics Model of a Small Flexible Aircraft
A Gupta - 2019 - search.proquest.com
The presence of aeroservoelastic effects in the flight dynamics of flexible aircraft presents
significant challenges in terms of performance degradation and instability. In order to …
significant challenges in terms of performance degradation and instability. In order to …