Validation of Aero-Load Estimator for Convair 880 Aircraft Flight Simulator Benchmark with Electro-Hydrostatic Actuators

Autor: Yamina BOUGHARI, Ruxandra Mihaela BOTEZ, Amir BANIAMERIAN, Ehsan SOBHANI TEHRANI, Armineh GARABEDIAN

Publikováno v: INCAS Bulletin, Vol 13, Iss 3, Pp 13-27 (2021)

Simulating an aircraft model using of high fidelity models of subsystems for its primary and secondary flight control actuators requires measuring or estimating aero-load data acting on flight control surfaces. One solution would be to incorporate th

Externí odkaz: https://doaj.org/article/83e6fda0ecda4aa2a62b6a31c830fa83

Validation of Aero-Load Estimator for Convair 880 Aircraft Flight Simulator Benchmark with Electro-Hydrostatic Actuators

Autor: Ehsan Sobhani Tehrani, Ruxandra Mihaela Botez, Amir Baniamerian, Yamina Boughari, Armineh Garabedian

Publikováno v: INCAS Bulletin, Vol 13, Iss 3, Pp 13-27 (2021)

Simulating an aircraft model using of high fidelity models of subsystems for its primary and secondary flight control actuators requires measuring or estimating aero-load data acting on flight control surfaces. One solution would be to incorporate th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7275d1997ea9c276eb33c1441d6131a2
https://doi.org/10.13111/2066-8201.2021.13.3.2

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Simulation of Cosmic Radiation Transport Inside Aircraft for Safety Applications

Autor: José M. Molina, Adriane Cristina Mendes Prado, M. T. Pazianotto, M. A. Cortés-Giraldo, C. A. Federico, Guillaume Hubert, Marlon Antonio Pereira

Publikováno v: IEEE Transactions on Aerospace and Electronic Systems
IEEE Transactions on Aerospace and Electronic Systems, Institute of Electrical and Electronics Engineers, 2020, 56 (5), pp.3462-3475. ⟨10.1109/taes.2020.2985304⟩

International audience; During the flight, an aircraft is submitted to a radiation environment composed of cosmic-ray-induced particles (CRIP) of which neutrons are responsible for approximately 40% of the crew effective dose and are the main cause o

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a2004ea5338fd43cd1527da7e4b36677
https://doi.org/10.1109/taes.2020.2985304

Unsteady Detached-Eddy Simulation (DES) of the Jetstream 31 aircraft in One Engine Inoperative (OEI) condition with propeller modelling

Autor: Loris Casadei, László Könözsy, Nicholas J. Lawson

Publikováno v: Aerospace Science and Technology. 91:287-300

Numerical results from a three-dimensional (3D) computational fluid dynamics (CFD) model of the Jetstream 31 aircraft in conditions of one engine inoperative are presented. The objective of this work is to analyse the performance of the Jetstream 31

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::13a4e868f0e1ccbf9947c3d53c753528
https://doi.org/10.1016/j.ast.2019.05.034