Cover Image
Read Now

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...

Full description

Bibliographic Details
Main Author: Botez, Ruxandra Mihaela
Other Authors: Grigorie, Teodor Lucian, Sugar-Gabor, Oliviu, Murrieta-Mendoza, Alejandro
Format: eBook
Language:English
Published: Basel MDPI - Multidisciplinary Digital Publishing Institute 2022
Subjects:
Computational Fluid Dynamics
Tailless Aircraft
Turbulence Modeling
Spin-up
Backward-facing Step Flow
Cascade Flow
N/a
Flight Tests
Stress Analysis
Fe Modeling
Flat Plate Flow
Pso
History Of Engineering And Technology / Bicssc
Aerodynamic Performance
Disturbance Observer
Technology: General Issues / Bicssc
Loads Assessment
Airfoil Flow
Wind Tunnel
Morphing Airfoil Optimization
Ground Loads
Landing Gear Dynamics
Oleo-pneumatic Shock Absorber
Parameterization
Adaptive Structures
Spring-back
Drop Impact
Nonlinear Dynamic Inversion
Anti-windup
Online Access:
Collection: Directory of Open Access Books - Collection details see MPG.ReNa
Description
Summary: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.
Item Description:Creative Commons (cc), https://creativecommons.org/licenses/by/4.0/
Physical Description:1 electronic resource (126 p.)
ISBN:books978-3-0365-3211-0
9783036532103
9783036532110

Similar Items