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...
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| Other Authors: | , , , |
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| Format: | Book Chapter |
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Basel
MDPI - Multidisciplinary Digital Publishing Institute
2022
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| Online Access: | Get Fullteks DOAB: description of the publication |
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| LEADER | 03020naaaa2200697uu 4500 | ||
|---|---|---|---|
| 001 | doab_20_500_12854_79648 | ||
| 005 | 20220321 | ||
| 020 | |a books978-3-0365-3211-0 | ||
| 020 | |a 9783036532103 | ||
| 020 | |a 9783036532110 | ||
| 024 | 7 | |a 10.3390/books978-3-0365-3211-0 |c doi | |
| 041 | 0 | |a English | |
| 042 | |a dc | ||
| 072 | 7 | |a TB |2 bicssc | |
| 072 | 7 | |a TBX |2 bicssc | |
| 100 | 1 | |a Botez, Ruxandra Mihaela |4 edt | |
| 700 | 1 | |a Grigorie, Teodor Lucian |4 edt | |
| 700 | 1 | |a Sugar-Gabor, Oliviu |4 edt | |
| 700 | 1 | |a Murrieta-Mendoza, Alejandro |4 edt | |
| 700 | 1 | |a Botez, Ruxandra Mihaela |4 oth | |
| 700 | 1 | |a Grigorie, Teodor Lucian |4 oth | |
| 700 | 1 | |a Sugar-Gabor, Oliviu |4 oth | |
| 700 | 1 | |a Murrieta-Mendoza, Alejandro |4 oth | |
| 245 | 1 | 0 | |a Aircraft Modeling and Simulation |
| 260 | |a Basel |b MDPI - Multidisciplinary Digital Publishing Institute |c 2022 | ||
| 300 | |a 1 electronic resource (126 p.) | ||
| 506 | 0 | |a Open Access |2 star |f Unrestricted online access | |
| 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 |4 https://creativecommons.org/licenses/by/4.0/ | ||
| 546 | |a English | ||
| 650 | 7 | |a Technology: general issues |2 bicssc | |
| 650 | 7 | |a History of engineering & technology |2 bicssc | |
| 653 | |a tailless aircraft | ||
| 653 | |a nonlinear dynamic inversion | ||
| 653 | |a disturbance observer | ||
| 653 | |a anti-windup | ||
| 653 | |a flight tests | ||
| 653 | |a wind tunnel | ||
| 653 | |a morphing airfoil optimization | ||
| 653 | |a parameterization | ||
| 653 | |a PSO | ||
| 653 | |a aerodynamic performance | ||
| 653 | |a computational fluid dynamics | ||
| 653 | |a turbulence modeling | ||
| 653 | |a flat plate flow | ||
| 653 | |a backward-facing step flow | ||
| 653 | |a airfoil flow | ||
| 653 | |a cascade flow | ||
| 653 | |a adaptive structures | ||
| 653 | |a FE modeling | ||
| 653 | |a stress analysis | ||
| 653 | |a loads assessment | ||
| 653 | |a landing gear dynamics | ||
| 653 | |a drop impact | ||
| 653 | |a oleo-pneumatic shock absorber | ||
| 653 | |a ground loads | ||
| 653 | |a spin-up | ||
| 653 | |a spring-back | ||
| 653 | |a n/a | ||
| 856 | 4 | 0 | |a www.oapen.org |u https://mdpi.com/books/pdfview/book/5033 |7 0 |z Get Fullteks |
| 856 | 4 | 0 | |a www.oapen.org |u https://directory.doabooks.org/handle/20.500.12854/79648 |7 0 |z DOAB: description of the publication |