On the public citation graph

Navier-Stokes applications to high-lift airfoil analysis

https://doi.org/10.2514/3.46764
0 signed · 52 inferred · view as graph

Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.

Is this your work? Sign in with ORCID and put your name on the claims that are yours.
Claim with ORCID
Reference health. See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.
See reference health

What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1002/fld.1650130905openalex-snapshot
Turbulent flow calculations using unstructured and adaptive meshes
inferredcites →https://doi.org/10.1017/s0001924000050971openalex-snapshot
Investigations into the effects of scale and compressibility on lift and drag in the RAE 5m pressurised low-speed wind tunnel
inferredcites →https://doi.org/10.2514/2.113openalex-snapshot
High-Lift Aerodynamic Computations with One- and Two-Equation Turbulence Models
inferredcites →https://doi.org/10.2514/3.11133openalex-snapshot
Three-dimensional unstructured multigrid for the Euler equations
inferredcites →https://doi.org/10.2514/3.25233openalex-snapshot
Multigrid solution of the Navier-Stokes equations on triangular meshes
inferredcites →https://doi.org/10.2514/6.1989-120openalex-snapshot
Multigrid solution of the Navier-Stokes equations on triangular meshes
inferredcites →https://doi.org/10.2514/6.1991-237openalex-snapshot
Multigrid solution of compressible turbulent flow on unstructured meshes using a two-equation model
inferredcites →https://doi.org/10.2514/6.1991-3332openalex-snapshot
Multi-element airfoil optimization for maximum lift at high Reynoldsnumbers
inferredcites →https://doi.org/10.2514/6.1992-4103openalex-snapshot
Subsonic high-lift flight research on the NASA Transport System Research Vehicle (TSRV)
inferredcites →https://doi.org/10.2514/6.1992-439openalex-snapshot
A one-equation turbulence model for aerodynamic flows
inferredcites →https://doi.org/10.2514/6.1993-2918openalex-snapshot
Surface hot-film method for the measurement of transition, separation and reattachment points

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.4776787openalex-extracted
Görtler Vortices Formation in Flow Over a Multi-Element Airfoil
inferred← citeshttps://doi.org/10.1002/(sici)1097-0363(19960930)23:6<527::aid-fld429>3.0.co;2-zopenalex-snapshot
A 3D AGGLOMERATION MULTIGRID SOLVER FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS ON UNSTRUCTURED MESHES
inferred← citeshttps://doi.org/10.1007/s10494-015-9656-7openalex-snapshot
A Spalart–allmaras Turbulence Model Implementation for High-order Discontinuous Galerkin Solution of the Reynolds-averaged Navier-stokes Equations
inferred← citeshttps://doi.org/10.1016/0045-7930(95)00005-wopenalex-snapshot
Agglomeration multigrid for two-dimensional viscous flows
inferred← citeshttps://doi.org/10.1016/j.cpc.2025.109833openalex-snapshot
GPU-based compressible lattice Boltzmann simulations on non-uniform grids using standard C++ parallelism: From best practices to aerodynamics, aeroacoustics and supersonic flow simulations
inferred← citeshttps://doi.org/10.1016/j.jcp.2009.07.013openalex-snapshot
Multigrid algorithms for high-order discontinuous Galerkin discretizations of the compressible Navier–Stokes equations
inferred← citeshttps://doi.org/10.1016/s0045-7930(97)00054-6openalex-snapshot
An interactive boundary-layer method for multielement airfoils
inferred← citeshttps://doi.org/10.1016/s0376-0421(02)00002-7openalex-snapshot
The aerodynamic design of multi-element high-lift systems for transport airplanes
inferred← citeshttps://doi.org/10.1016/s0376-0421(02)00003-9openalex-snapshot
Prediction of high lift: review of present CFD capability
inferred← citeshttps://doi.org/10.1063/5.0036088openalex-snapshot
Slat cove dynamics of low Reynolds number flow past a 30P30N high lift configuration
inferred← citeshttps://doi.org/10.2514/1.29924openalex-snapshot
Unsteady Discrete Adjoint Formulation for Two-Dimensional Flow Problems with Deforming Meshes
inferred← citeshttps://doi.org/10.2514/1.j054534openalex-snapshot
Mesh-Resolved Airfoil Simulations Using Finite Volume and Discontinuous Galerkin Solvers
inferred← citeshttps://doi.org/10.2514/1.j063929openalex-snapshot
Identifying Buffet Oscillations Using Sliding-Window Dynamic Mode Decomposition
inferred← citeshttps://doi.org/10.2514/2.113openalex-snapshot
High-Lift Aerodynamic Computations with One- and Two-Equation Turbulence Models
inferred← citeshttps://doi.org/10.2514/2.2517openalex-snapshot
Computational Investigation of Simulated Large-Droplet Ice Shapes on Airfoil Aerodynamics
inferred← citeshttps://doi.org/10.2514/2.435openalex-snapshot
Prediction of High-Lift Flows Using Turbulent Closure Models
inferred← citeshttps://doi.org/10.2514/2.894openalex-snapshot
Viscous Flow Analysis Using a Parallel Unstructured Multigrid Solver
inferred← citeshttps://doi.org/10.2514/3.13101openalex-snapshot
Perspective on unstructured grid flow solvers
inferred← citeshttps://doi.org/10.2514/6.1994-1878openalex-snapshot
A three dimensional multigrid Reynolds-averaged Navier-Stokes solver for unstructured meshes
inferred← citeshttps://doi.org/10.2514/6.1994-2332openalex-snapshot
Agglomeration multigrid for viscous turbulent flows
inferred← citeshttps://doi.org/10.2514/6.1995-43openalex-snapshot
Viscous-flow analysis of a subsonic transport high-lift system including comparisons with flight-measured results
inferred← citeshttps://doi.org/10.2514/6.1995-667openalex-snapshot
A perspective on unstructured grid flow solvers
inferred← citeshttps://doi.org/10.2514/6.1996-57openalex-snapshot
Evaluation of turbulence models for high-lift military airfoil flowfields
inferred← citeshttps://doi.org/10.2514/6.1997-2232openalex-snapshot
Design of high-lift airfoils for low aspect ratio wings with endplates
inferred← citeshttps://doi.org/10.2514/6.1998-2619openalex-snapshot
Three-dimensional high-lift analysis using a parallel, unstructured multigrid solver
inferred← citeshttps://doi.org/10.2514/6.1999-93openalex-snapshot
Effects of simulated-spanwise-ice shapes on airfoils - Computational investigation
inferred← citeshttps://doi.org/10.2514/6.2005-1355openalex-snapshot
A Numerical Parametric Study of High-Lift Low Reynolds Number Airfoils
inferred← citeshttps://doi.org/10.2514/6.2005-4711openalex-snapshot
Farfield Boundary Conditions for 2-D Airfoils
inferred← citeshttps://doi.org/10.2514/6.2008-327openalex-snapshot
Aerodynamic Shape Optimization of Multi-Element Airfoils in Ground Effect
inferred← citeshttps://doi.org/10.2514/6.2012-457openalex-snapshot
Robust Computation of Turbulent Flows Using a Discontinuous Galerkin Method
inferred← citeshttps://doi.org/10.2514/6.2014-0554openalex-snapshot
Adjoint-based Shape Optimization of High-lift Airfoil using the NSU2D Unstructured Mesh Solver
inferred← citeshttps://doi.org/10.2514/6.2014-2701openalex-snapshot
A Time-Lag Approach for Prediction of Trailing Edge Separation in Unsteady Flow
inferred← citeshttps://doi.org/10.2514/6.2017-1224openalex-snapshot
Finite-element solutions to the Reynolds Averaged Navier-Stokes equations using a Spalart-Allmaras Turbulence Model
inferred← citeshttps://doi.org/10.2514/6.2018-0813openalex-snapshot
Low-Order Modeling of Airfoils with Massively Separated Flow and Leading-Edge Vortex Shedding
inferred← citeshttps://doi.org/10.2514/6.2022-1678openalex-snapshot
Comparison of Propeller-Wing Interaction Simulation using Different Levels of Fidelity
inferred← citeshttps://doi.org/10.2514/6.2022-2536openalex-snapshot
Coupled Analysis of a Slotted Natural-Laminar-Flow Transonic Truss-Braced Wing Aircraft Configuration
inferred← citeshttps://doi.org/10.2514/6.2023-2454openalex-snapshot
Effect of Transition Modeling for Analysis of a Slotted, Natural-Laminar-Flow Transonic Truss-Braced Wing Aircraft Configuration
inferred← citeshttps://doi.org/10.3390/aerospace12030251openalex-snapshot
The History of the Slotted Natural-Laminar-Flow Airfoil for Improved Fuel Efficiency
inferred← citeshttps://doi.org/10.3390/jeta2040010openalex-snapshot
On the Origin of Görtler Vortices in Flow over a Multi-Element Airfoil
inferred← citeshttps://doi.org/10.4050/vfs-f68-000292openalex-snapshot
Adjoint-Based Unsteady Airfoil Design Optimization with Application to Dynamic Stall
inferred← citeshttps://doi.org/10.70675/df3370e1z5faaz4b6azab27z0c8d1667dc5fopenalex-snapshot
Towards the computational prediction of low-speed buffet : improved wall modeling for the Lattice Boltzmann method
Editorial review for independent work. ICSAC — the Institute for Complexity Science and Advanced Computing — runs a structured editorial panel for researchers publishing outside journals, and publishes on CiteStamp rails. Submission is free and goes through ORCID: icsacinstitute.org/submit.