[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Rahmani et al., 2022 - Google Patents

Comparison of low-and high-order CFD based estimates of forces, moments and aerodynamic coefficients with UAS flight test data

Rahmani et al., 2022

Document ID
14738948390488798424
Author
Rahmani S
Wang Z
Matt J
Chao H
Zheng C
Publication year
Publication venue
AIAA AVIATION 2022 Forum

External Links

Snippet

View Video Presentation: https://doi. org/10.2514/6.2022-4065. vid The aerodynamic coefficients and stability derivatives generated by a variety of low-and-high fidelity computational simulations were compared to flight test. It was found that at zero angle of …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5095Vehicle design, e.g. aircraft or automotive design
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06Frames; Stringers; Longerons; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/46Fuselage

Similar Documents

Publication Publication Date Title
Crozon et al. Coupled flight dynamics and CFD–demonstration for helicopters in shipborne environment
Keye Fluid-structure coupled analysis of a transport aircraft and flight-test validation
Slotnick Computational aerodynamic analysis for the formation flight for aerodynamic benefit program
Smith et al. Longitudinal aerodynamic modeling of the adaptive compliant trailing edge flaps on a GIII aircraft and comparisons to flight data
Bizinos et al. Tentative study of passenger comfort during formation flight within atmospheric turbulence
Mavriplis et al. Supersonic Configurations at Low Speeds (SCALOS): CFD Aided Wind Tunnel Data Corrections
Tomac et al. Engineering methods applied to an unmanned combat air vehicle configuration
Herrmann et al. Nonlinear system identification of a UAV model with distributed aerodynamics and flexible structure
Shafer et al. Comparison of computational approaches for rapid aerodynamic assessment of small UAVs
Duca et al. Effects of epistemic uncertainty on empennage loads during dynamic maneuvers
Rahmani et al. Comparison of low-and high-order CFD based estimates of forces, moments and aerodynamic coefficients with UAS flight test data
Clifton et al. Determining the stability and control characteristics of high-performance maneuvering aircraft using high-resolution CFD simulation with and without moving control surfaces
Duncan Jr The effects of step excrescences on swept-wing boundary-layer transition
Wu et al. An approach to estimate aircraft touchdown attitudes and control inputs
Chyczewski et al. A position on current stability and control prediction capabilities and a path forward
Herrmann et al. System identification of a nonlinear uav model with distributed aerodynamics and flexible structure
Venkatachari et al. Boundary-Layer Transition Prediction Through Loose Coupling of OVERFLOW and LASTRAC
Morton et al. CFD-Based Reduced-Order Models of F-16XL Static and Dynamic Loads Using Kestrel
Cruz et al. Evaluation of Load Analysis Methods for NASA’ s GIII Adaptive Compliant Trailing Edge Project
Kernazhitskiy et al. Modeling and Simulation of the Effects of Underwing Aerodynamics on Flutter Evaluation of the F-16 Aircraft
Götten et al. Full Configuration Drag Estimation of Small-to-Medium Range UAVs and Its Impact on Initial Sizing Optimization
Livne Supersonic Configurations at Low Speeds (SCALOS): CFD Aided Wind Tunnel Data Corrections
Harrison et al. Investigation and Flight Dynamic Analysis of General Aviation Safety
Almosnino Assessment of an Inviscid Euler-Adjoint Solver for Prediction of Aerodynamic Characteristics of the NASA HL-20 Lifting Body
Klausmeyer Stability derivative estimation: Methods and practical considerations for conventional transonic aircraft