Nothing Special   »   [go: up one dir, main page]

Stebbins et al., 2022 - Google Patents

Computational analysis of the wake structure of a swept-wing

Stebbins et al., 2022

Document ID
2787754864797252227
Author
Stebbins S
Loth E
Publication year
Publication venue
AIAA SCITECH 2022 Forum

External Links

Snippet

View Video Presentation: https://doi. org/10.2514/6.2022-1170. vid Recent experimental work completed has sought to develop experimental techniques to capture effects on the flowfield downstream of a model in a wind tunnel. These techniques focused on utilizing a …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5095—Vehicle design, e.g. aircraft or automotive design
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00—Indexing scheme relating to computer aided design [CAD]
    • G06F2217/46—Fuselage
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00—Indexing scheme relating to computer aided design [CAD]
    • G06F2217/16—Numerical modeling
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00—Indexing scheme relating to computer aided design [CAD]
    • G06F2217/80—Thermal analysis and optimization
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing

Similar Documents

Publication Publication Date Title
Levy et al. Summary of data from the fifth computational fluid dynamics drag prediction workshop
Slotnick et al. Overview of the 1st AIAA CFD high lift prediction workshop
Brune Quantitative low-speed wake surveys
Halila et al. Effects of boundary layer transition on the aerodynamic analysis of high-lift systems
Arntz et al. Exergy-based performance assessment of the NASA common research model
Pettersson et al. Aerodynamic scaling to free flight conditions: Past and present
Mader et al. Computation of aircraft stability derivatives using an automatic differentiation adjoint approach
Ribeiro et al. Direct numerical simulation of an airfoil with sand grain roughness on the leading edge
Frink et al. Collaborative study of incipient separation on 53-swept diamond wing
Wokoeck et al. RANS simulation and experiments on the stall behaviour of an airfoil with laminar separation bubbles
Sclafani et al. Extended OVERFLOW analysis of the NASA trap wing wind tunnel model
Giannelis et al. Rigid buffet response of the benchmark supercritical wing for the third aeroelastic prediction workshop
Ghoreyshi et al. Framework for establishing limits of tabular aerodynamic models for flight dynamics analysis
Ranzenbach et al. Multi-element airfoil in ground effect-an experimental and computational study
Coder Standard test cases for CFD-based laminar-transition model verification and validation
Guillermo-Monedero A comparison of Euler finite volume and supersonic vortex lattice methods used during the conceptual design phase of supersonic delta wings
Stebbins et al. Computational analysis of the wake structure of a swept-wing
Stebbins et al. Computations of swept wing icing aerodynamics
Lei et al. CFD validation for high-lift devices: two-element airfoil
Müller et al. Numerical simulation of the swept FNG wing in atmospheric turbulence
Whitehouse et al. Development and testing of a low cost CFD based analysis for surface mesh interrogation & refinement for applied aerodynamics applications
Samuell Development of a turbulent separated flow validation test case: Experimental and computational (RANS) studies
Craig Penner et al. Wall-Modeled Large-Eddy Simulations of a Swept Wing with Leading-Edge Ice
Souverein et al. Particle image velocimetry based loads determination in supersonic flows
Elmiligui et al. Sonic boom computations for a mach 1.6 cruise low boom configuration and comparisons with wind tunnel data