02808nam 2200709z- 450 991055761990332120220321(CKB)5400000000045218(oapen)https://directory.doabooks.org/handle/20.500.12854/79648(oapen)doab79648(EXLCZ)99540000000004521820202203d2022 |y 0engurmn|---annantxtrdacontentcrdamediacrrdacarrierAircraft Modeling and SimulationBaselMDPI - Multidisciplinary Digital Publishing Institute20221 online resource (126 p.)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.History of engineering and technologybicsscTechnology: general issuesbicsscadaptive structuresaerodynamic performanceairfoil flowanti-windupbackward-facing step flowcascade flowcomputational fluid dynamicsdisturbance observerdrop impactFE modelingflat plate flowflight testsground loadslanding gear dynamicsloads assessmentmorphing airfoil optimizationn/anonlinear dynamic inversionoleo-pneumatic shock absorberparameterizationPSOspin-upspring-backstress analysistailless aircraftturbulence modelingwind tunnelHistory of engineering and technologyTechnology: general issuesGrigorie Teodor LucianSugar-Gabor OliviuMurrieta-Mendoza AlejandroBotez Ruxandra MihaelaBOOK9910557619903321Aircraft Modeling and Simulation3027106UNINA