LEADER 02712nam  2200685z- 450 
001 9910557619903321
005 20231214133348.0
035   $a(CKB)5400000000045218
035   $a(oapen)https://directory.doabooks.org/handle/20.500.12854/79648
035   $a(EXLCZ)995400000000045218
100   $a20202203d2022      |y             0
101 0 $aeng
135   $aurmn|---annan
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aAircraft Modeling and Simulation
210   $aBasel$cMDPI - Multidisciplinary Digital Publishing Institute$d2022
215   $a1 electronic resource (126 pages)
311   $a3-0365-3210-2 
311   $a3-0365-3211-0 
330   $aVarious 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.
606   $aTechnology$xHistory
606   $aEngineering$xHistory
610   $atailless aircraft
610   $anonlinear dynamic inversion
610   $adisturbance observer
610   $aanti-windup
610   $aflight tests
610   $awind tunnel
610   $amorphing airfoil optimization
610   $aparameterization
610   $aPSO
610   $aaerodynamic performance
610   $acomputational fluid dynamics
610   $aturbulence modeling
610   $aflat plate flow
610   $abackward-facing step flow
610   $aairfoil flow
610   $acascade flow
610   $aadaptive structures
610   $aFE modeling
610   $astress analysis
610   $aloads assessment
610   $alanding gear dynamics
610   $adrop impact
610   $aoleo-pneumatic shock absorber
610   $aground loads
610   $aspin-up
610   $aspring-back
615  0$aTechnology$xHistory.
615  0$aEngineering$xHistory.
702   $aGrigorie$b Teodor Lucian
702   $aSugar-Gabor$b Oliviu
702   $aMurrieta-Mendoza$b Alejandro
702   $aBotez$b Ruxandra Mihaela
906   $aBOOK
912   $a9910557619903321
996   $aAircraft Modeling and Simulation$93027106
997   $aUNINA