Aircraft Modeling and Simulation
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...
| Format: | eBook |
|---|---|
| Language: | English |
| Published: |
Basel
MDPI - Multidisciplinary Digital Publishing Institute
2022
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| Subjects: | |
| Online Access: | Open Access: DOAB: description of the publication Open Access: DOAB, download the publication |
| LEADER | 03326namaa2200805uu 4500 | ||
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| 024 | 7 | |a 10.3390/books978-3-0365-3211-0 |2 doi | |
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| 072 | 7 | |a TB |2 bicssc | |
| 072 | 7 | |a TBX |2 bicssc | |
| 720 | 1 | |a Botez, Ruxandra Mihaela |4 edt | |
| 720 | 1 | |a Botez, Ruxandra Mihaela |4 oth | |
| 720 | 1 | |a Grigorie, Teodor Lucian |4 edt | |
| 720 | 1 | |a Grigorie, Teodor Lucian |4 oth | |
| 720 | 1 | |a Murrieta-Mendoza, Alejandro |4 edt | |
| 720 | 1 | |a Murrieta-Mendoza, Alejandro |4 oth | |
| 720 | 1 | |a Sugar-Gabor, Oliviu |4 edt | |
| 720 | 1 | |a Sugar-Gabor, Oliviu |4 oth | |
| 245 | 0 | 0 | |a Aircraft Modeling and Simulation |
| 260 | |a Basel |b MDPI - Multidisciplinary Digital Publishing Institute |c 2022 | ||
| 300 | |a 1 online resource (126 p.) | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 506 | 0 | |a Open Access |f Unrestricted online access |2 star | |
| 520 | |a 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. | ||
| 540 | |a Creative Commons |f https://creativecommons.org/licenses/by/4.0/ |2 cc |u https://creativecommons.org/licenses/by/4.0/ | ||
| 546 | |a English | ||
| 650 | 7 | |a History of engineering and technology |2 bicssc | |
| 650 | 7 | |a Technology: general issues |2 bicssc | |
| 653 | |a adaptive structures | ||
| 653 | |a aerodynamic performance | ||
| 653 | |a airfoil flow | ||
| 653 | |a anti-windup | ||
| 653 | |a backward-facing step flow | ||
| 653 | |a cascade flow | ||
| 653 | |a computational fluid dynamics | ||
| 653 | |a disturbance observer | ||
| 653 | |a drop impact | ||
| 653 | |a FE modeling | ||
| 653 | |a flat plate flow | ||
| 653 | |a flight tests | ||
| 653 | |a ground loads | ||
| 653 | |a landing gear dynamics | ||
| 653 | |a loads assessment | ||
| 653 | |a morphing airfoil optimization | ||
| 653 | |a n/a | ||
| 653 | |a nonlinear dynamic inversion | ||
| 653 | |a oleo-pneumatic shock absorber | ||
| 653 | |a parameterization | ||
| 653 | |a PSO | ||
| 653 | |a spin-up | ||
| 653 | |a spring-back | ||
| 653 | |a stress analysis | ||
| 653 | |a tailless aircraft | ||
| 653 | |a turbulence modeling | ||
| 653 | |a wind tunnel | ||
| 793 | 0 | |a DOAB Library. | |
| 856 | 4 | 0 | |u https://directory.doabooks.org/handle/20.500.12854/79648 |7 0 |z Open Access: DOAB: description of the publication |
| 856 | 4 | 0 | |u https://mdpi.com/books/pdfview/book/5033 |7 0 |z Open Access: DOAB, download the publication |