02712nam 2200685z- 450 991055761990332120231214133348.0(CKB)5400000000045218(oapen)https://directory.doabooks.org/handle/20.500.12854/79648(EXLCZ)99540000000004521820202203d2022 |y 0engurmn|---annantxtrdacontentcrdamediacrrdacarrierAircraft Modeling and SimulationBaselMDPI - Multidisciplinary Digital Publishing Institute20221 electronic resource (126 pages)3-0365-3210-2 3-0365-3211-0 Various aerodynamics, structural dynamics, and control design and experimental studies are presented with the aim of advancing green and morphing aircraft research. The results obtained with an in-house CFD code are compared and validated with those of two NASA codes. The aerodynamical model of the UAS-S45 morphing wing as well as the structural model of a morphing winglet are presented. A new design methodology for oleo-pneumatic landing gear drop impact dynamics is presented as well as its experimental validation. The design of a nonlinear dynamic inversion (NDI)-based disturbance rejection control on a tailless aircraft is presented, including its validation using wind tunnel tests.TechnologyHistoryEngineeringHistorytailless aircraftnonlinear dynamic inversiondisturbance observeranti-windupflight testswind tunnelmorphing airfoil optimizationparameterizationPSOaerodynamic performancecomputational fluid dynamicsturbulence modelingflat plate flowbackward-facing step flowairfoil flowcascade flowadaptive structuresFE modelingstress analysisloads assessmentlanding gear dynamicsdrop impactoleo-pneumatic shock absorberground loadsspin-upspring-backTechnologyHistory.EngineeringHistory.Grigorie Teodor LucianSugar-Gabor OliviuMurrieta-Mendoza AlejandroBotez Ruxandra MihaelaBOOK9910557619903321Aircraft Modeling and Simulation3027106UNINA