Zobrazeno 1 - 10
of 192
pro vyhledávání: '"Pierangelo Masarati"'
Autor:
Simone Conti, Emanuel Tschopp, Octávio Mateus, Andrea Zanoni, Pierangelo Masarati, Giuseppe Sala
Publikováno v:
Scientific Reports, Vol 12, Iss 1, Pp 1-9 (2022)
Abstract Sauropod dinosaurs are well known for their massive sizes and long necks and tails. Among sauropods, flagellicaudatan dinosaurs are characterized by extreme tail elongation, which has led to hypotheses regarding tail function, often compared
Externí odkaz:
https://doaj.org/article/cab97c116f354f9abd3aae5ba14a1ec1
Publikováno v:
International Journal of Mechanical System Dynamics, Vol 1, Iss 1, Pp 108-120 (2021)
Abstract A generalized solution scheme using implicit time integrators for piecewise linear and nonlinear systems is developed. The piecewise linear characteristic has been well‐discussed in previous studies, in which the original problem has been
Externí odkaz:
https://doaj.org/article/3e4534c8af6f4be8a971a9b000d53cf3
Publikováno v:
Sensors, Vol 23, Iss 14, p 6308 (2023)
Sensing the interaction between the pilot and the control inceptors can provide important information about the pilot’s activity during flight, potentially enabling the objective measurement of the pilot workload, the application of preventive acti
Externí odkaz:
https://doaj.org/article/d8f1d96874ec457794e10d71f1b77a55
Publikováno v:
Vibration, Vol 4, Iss 1, Pp 133-150 (2021)
Helicopters are known to exhibit higher vibratory levels compared to fixed-wing aircraft. The consequences of vibrations depend on the affected helicopter component or subject. Specifically, pilots are in contact with several parts of the helicopter;
Externí odkaz:
https://doaj.org/article/dff7b2c6e4f945cf9ac657cdc4aad5bb
Autor:
Aykut Tamer, Pierangelo Masarati
Publikováno v:
Aerospace, Vol 9, Iss 1, p 10 (2021)
Rotorcraft stability is an inherently multidisciplinary area, including aerodynamics of rotor and fuselage, structural dynamics of flexible structures, actuator dynamics, control, and stability augmentation systems. The related engineering models can
Externí odkaz:
https://doaj.org/article/2e1fd70c066b4cacbecc29424f03cbe2
Autor:
Alberto Savino, Alessandro Cocco, Alex Zanotti, Matteo Tugnoli, Pierangelo Masarati, Vincenzo Muscarello
Publikováno v:
Energies, Vol 14, Iss 21, p 6979 (2021)
A mid-fidelity aerodynamic solver based on the vortex particle method for wake modeling, DUST, is coupled through the partitioned multi-physics coupling library preCICE to a multibody dynamics code, MBDyn, to improve the accuracy of aeroelastic numer
Externí odkaz:
https://doaj.org/article/a7cf0f6deb6349cebee91012a34a9fa0
Publikováno v:
Sensors, Vol 20, Iss 15, p 4196 (2020)
The interaction between the rotating blades and the external fluid in non-axial flow conditions is the main source of vibratory loads on the main rotor of helicopters. The knowledge or prediction of the produced aerodynamic loads and of the dynamic b
Externí odkaz:
https://doaj.org/article/fdb3121027f14ab6a5e19420f834c96a
Publikováno v:
Aerospace, Vol 7, Iss 5, p 59 (2020)
Helicopter Emergency and Medical Service (HEMS) vehicles require a specially configured cabin that supports the quick transport of a rescue team to the site of an emergency and return of patients back to a full capacity hospital, while sustaining the
Externí odkaz:
https://doaj.org/article/8a91f336dc8644469960bf2f4bc044b7
Publikováno v:
Multibody System Dynamics. 57:237-257
The formulation of constrained system dynamics using coordinate projection onto a subspace locally tangent to the constraint manifold is revisited using the QR factorization of the constraint Jacobian matrix to extract a suitable subspace and integra
Publikováno v:
CEAS Aeronautical Journal. 13:923-938
This work presents the modeling and preliminary Whirl–Flutter stability results achieved within the Advanced Testbed for TILtrotor Aeroelastics (ATTILA) CleanSky2 project. The project addresses the design, manufacturing, and testing of a semi-span