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Computational Aerodynamic Modeling of Aerospace Vehicles



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Autore: Jenkins Karl Visualizza persona
Titolo: Computational Aerodynamic Modeling of Aerospace Vehicles Visualizza cluster
Pubblicazione: MDPI - Multidisciplinary Digital Publishing Institute, 2019
Descrizione fisica: 1 online resource (294 p.)
Soggetto topico: History of engineering and technology
Soggetto non controllato: aerodynamic performance
aerodynamics
aeroelasticity
after-body
angle of attack
bifurcation
bluff body
CFD
characteristics-based scheme
chemistry
computational fluid dynamics
computational fluid dynamics (CFD)
convolution integral
CPACS
DDES
detection
discontinuous Galerkin finite element method (DG-FEM)
dynamic Smagorinsky subgrid-scale model
Euler
flexible wings
flow control
flow distortion
fluid mechanics
flutter
formation
gasdynamics
geometry
Godunov method
high angles of attack
hybrid reduced-order model
hypersonic
installed propeller
kinetic energy dissipation
large eddy simulation
MDO
meshing
microelectromechanical systems (MEMS)
microfluidics
modeling
modified equation analysis
multi-directional
multi-fidelity
MUSCL
neural networks
numerical dissipation
numerical methods
overset grid approach
p-factor
quasi-analytical
RANS
reduced order aerodynamic model
reduced-order model
Riemann solver
S-duct diffuser
sharp-edge gust
shock-channel
slender-body
square cylinder
subsonic
Taylor-Green vortex
truncation error
turbulence model
unsteady aerodynamic characteristics
URANS
variable fidelity
VLM
vortex generators
wake
wind gust responses
wind tunnel
wing-propeller aerodynamic interaction
Persona (resp. second.): GhoreyshiMehdi
Sommario/riassunto: Currently, the use of computational fluid dynamics (CFD) solutions is considered as the state-of-the-art in the modeling of unsteady nonlinear flow physics and offers an early and improved understanding of air vehicle aerodynamics and stability and control characteristics. This Special Issue covers recent computational efforts on simulation of aerospace vehicles including fighter aircraft, rotorcraft, propeller driven vehicles, unmanned vehicle, projectiles, and air drop configurations. The complex flow physics of these configurations pose significant challenges in CFD modeling. Some of these challenges include prediction of vortical flows and shock waves, rapid maneuvering aircraft with fast moving control surfaces, and interactions between propellers and wing, fluid and structure, boundary layer and shock waves. Additional topic of interest in this Special Issue is the use of CFD tools in aircraft design and flight mechanics. The problem with these applications is the computational cost involved, particularly if this is viewed as a brute-force calculation of vehicle's aerodynamics through its flight envelope. To make progress in routinely using of CFD in aircraft design, methods based on sampling, model updating and system identification should be considered.
Titolo autorizzato: Computational Aerodynamic Modeling of Aerospace Vehicles  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910346677003321
Lo trovi qui: Univ. Federico II
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