On the public citation graph

Numerical study of flows past airfoils with wavy surfaces

https://doi.org/10.1016/j.jfluidstructs.2012.09.008

0 signed · 95 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 See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.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/10.1006/jfls.1997.0128openalex-snapshot

REDUCTION OF BLUFF-BODY DRAG AND SUPPRESSION OF VORTEX SHEDDING BY THE INTRODUCTION OF WAVY SEPARATION LINES

inferredcites →https://doi.org/10.1007/s003480050250openalex-snapshot

Direct measurement of circulation using ultrasound

inferredcites →https://doi.org/10.1016/0021-9991(86)90099-9openalex-snapshot

Solution of the implicitly discretised fluid flow equations by operator-splitting

inferredcites →https://doi.org/10.1016/j.compfluid.2005.10.004openalex-snapshot

Large eddy simulation of pulsating flow over a circular cylinder at subcritical Reynolds number

inferredcites →https://doi.org/10.1016/j.compfluid.2007.04.008openalex-snapshot

Aerodynamic noise simulation of the flow past an airfoil trailing-edge using a hybrid zonal RANS-LES

inferredcites →https://doi.org/10.1016/j.compfluid.2007.10.010openalex-snapshot

Numerical study of passive and active flow separation control over a NACA0012 airfoil

inferredcites →https://doi.org/10.1016/j.ijheatfluidflow.2005.08.007openalex-snapshot

Computation of unsteady flow and aerodynamic noise of NACA0018 airfoil using large-eddy simulation

inferredcites →https://doi.org/10.1016/j.ijheatfluidflow.2008.01.006openalex-snapshot

Large eddy simulation of flow around wavy cylinders at a subcritical Reynolds number

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2005.08.009openalex-snapshot

An investigation on the lift force of a wing pitching in dynamic stall for a comfort control vessel

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2008.07.004openalex-snapshot

Anisotropic Organised Eddy Simulation for the prediction of non-equilibrium turbulent flows around bodies

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2010.07.005openalex-snapshot

Investigation of turbulent flow past a yawed wavy cylinder

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2010.07.006openalex-snapshot

Numerical study of turbulent trailing-edge flows with base cavity effects using URANS

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2012.04.003openalex-snapshot

High-order simulations of low Reynolds number membrane airfoils under prescribed motion

inferredcites →https://doi.org/10.1016/j.jfluidstructs.2012.04.011openalex-snapshot

Turbulence modeling of deep dynamic stall at relatively low Reynolds number

inferredcites →https://doi.org/10.1016/s0889-9746(03)00018-5openalex-snapshot

Simulation of dynamic stall for a NACA 0012 airfoil using a vortex method

inferredcites →https://doi.org/10.1017/s0022112000002299openalex-snapshot

Flow past a square-section cylinder with a wavy stagnation face

inferredcites →https://doi.org/10.1017/s0022112006001364openalex-snapshot

Drag reduction in flow over a two-dimensional bluff body with a blunt trailing edge using a new passive device

inferredcites →https://doi.org/10.1017/s0022112008000864openalex-snapshot

Direct numerical simulations of forced and unforced separation bubbles on an airfoil at incidence

inferredcites →https://doi.org/10.1017/s0022112008004217openalex-snapshot

Effects of wavelength and amplitude of a wavy cylinder in cross-flow at low Reynolds numbers

inferredcites →https://doi.org/10.1017/s0022112096003631openalex-snapshot

A study of three-dimensional aspects of vortex shedding from a bluff body with a mild geometric disturbance

inferredcites →https://doi.org/10.1088/1468-5248/5/1/019openalex-snapshot

Active control of turbulent flow over a model vehicle for drag reduction

inferredcites →https://doi.org/10.1088/1468-5248/5/1/037openalex-snapshot

Large eddy simulation and experimental study of flashback and blow-off in a lean partially premixed swirled burner

inferredcites →https://doi.org/10.1115/1.1427927openalex-snapshot

Computational Evaluation of the Periodic Performance of a NACA 0012 Fitted With a Gurney Flap

inferredcites →https://doi.org/10.1115/1.4000741openalex-snapshot

Computational Investigation of a Race Car Wing With Vortex Generators in Ground Effect

inferredcites →https://doi.org/10.1146/annurev.fl.23.010191.000433openalex-snapshot

Drag Reduction In Nature

inferredcites →https://doi.org/10.1146/annurev.fluid.35.101101.161102openalex-snapshot

A ERODYNAMICS OF S MALL V EHICLES

inferredcites →https://doi.org/10.1175/1520-0493(1963)091<0099:gcewtp>2.3.co;2openalex-snapshot

GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS

inferredcites →https://doi.org/10.2514/1.18969openalex-snapshot

Aerodyamic Flow Control of an Airfoil with Small Trailing-Edge Strips

inferredcites →https://doi.org/10.2514/1.2255openalex-snapshot

Numerical Study of Blowing and Suction Control Mechanism on NACA0012 Airfoil

inferredcites →https://doi.org/10.2514/1.31995openalex-snapshot

Lift Enhancement by Static Extended Trailing Edge

inferredcites →https://doi.org/10.2514/1.43379openalex-snapshot

Aerodynamic Modification of NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap

inferredcites →https://doi.org/10.2514/1.j050133openalex-snapshot

Numerical Simulation on Plasma Circulation Control Airfoil

inferredcites →https://doi.org/10.2514/2.2673openalex-snapshot

Flow Control for an Airfoil with Leading-Edge Rotation: An Experimental Study

inferredcites →https://doi.org/10.2514/3.12557openalex-snapshot

Effect of ice on airfoil stall at high Reynolds numbers

inferredcites →https://doi.org/10.2514/3.12561openalex-snapshot

Vortex shedding and shear-layer instability of wing at low-Reynolds numbers

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.4806241openalex-extracted

Two- to Three-Dimensional Wake Transition Mechanism Induced by the Angle of Attack of a Naca0012 Airfoil

inferred← citeshttps://doi.org/10.1007/978-981-16-0159-0_37openalex-snapshot

Numerical Modelling and Simulation of Wind Turbine Blade Aerofoil for Performance Enhancement

inferred← citeshttps://doi.org/10.1007/978-981-96-6235-7_53openalex-snapshot

Active Flow Control of Sinusoidal Leading-Edge Airfoil Based on DBD Plasma

inferred← citeshttps://doi.org/10.1007/s00348-014-1710-zopenalex-snapshot

Experimental study of flow separation control on a low-Re airfoil using leading-edge protuberance method

inferred← citeshttps://doi.org/10.1007/s00348-025-03960-yopenalex-snapshot

Plasma-based anti-/de-icing: an experimental study utilizing supercooled water droplet image velocimetry

inferred← citeshttps://doi.org/10.1007/s13762-021-03784-3openalex-snapshot

A comprehensive review of the application of bio-inspired tubercles on the horizontal axis wind turbine blade

inferred← citeshttps://doi.org/10.1007/s40435-026-02010-7openalex-snapshot

Advances in aircraft aerodynamic analysis: a review of experimental, computational, and hybrid techniques

inferred← citeshttps://doi.org/10.1007/s40997-019-00313-zopenalex-snapshot

Investigations of Flow Phenomena Over a Flat Plate and NACA0012 Airfoil at High Angles of Attack

inferred← citeshttps://doi.org/10.1007/s42235-020-0067-7openalex-snapshot

Effects of Bionic Volute Tongue on Aerodynamic Performance and Noise Characteristics of Centrifugal Fan Used in the Air-conditioner

inferred← citeshttps://doi.org/10.1016/j.apacoust.2020.107311openalex-snapshot

Experimental study on noise reduction of a wavy multi-copter rotor

inferred← citeshttps://doi.org/10.1016/j.ast.2019.04.002openalex-snapshot

Numerical investigation on the biomimetic trailing edge of a high-subsonic turbine blade

inferred← citeshttps://doi.org/10.1016/j.ast.2020.106216openalex-snapshot

Aerodynamic performance and wake development of airfoils with wavy leading edges

inferred← citeshttps://doi.org/10.1016/j.egypro.2015.07.826openalex-snapshot

CFD Simulation of Turbulent Flow and Heat Transfer Over Rough Surfaces

inferred← citeshttps://doi.org/10.1016/j.enconman.2024.119178openalex-snapshot

The effects of the location of the leading-edge tubercles on the performance of horizontal axis wind turbine

inferred← citeshttps://doi.org/10.1016/j.euromechflu.2018.07.017openalex-snapshot

Numerical study of unsteady flows past a rotating wavy cylinder

inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2025.111604openalex-snapshot

Aerodynamic performance analysis of a NACA 63(4)-421 airfoil equipped with a trailing edge slot at suction side

inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2025.111681openalex-snapshot

Vortex dynamics of novel whale-biomimetic and conventional wings: Influence of aspect ratio on tip and fragmented flow structures

inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2026.110421openalex-snapshot

Electroactive morphing through spanwise travelling waves applied on an A320 wing by numerical simulation at Reynolds number 1 million

inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2015.12.004openalex-snapshot

Effects of large spanwise wavelength on the wake of a sinusoidal wavy cylinder

inferred← citeshttps://doi.org/10.1016/j.jsv.2016.11.021openalex-snapshot

Numerical study on reduction of aerodynamic noise around an airfoil with biomimetic structures

inferred← citeshttps://doi.org/10.1016/j.matpr.2020.05.564openalex-snapshot

CFD analysis of horizontal axis wind turbine braking system using chordwise spacing

inferred← citeshttps://doi.org/10.1016/j.matpr.2020.06.334openalex-snapshot

Aerodynamic braking system analysis of horizontal axis wind turbine using slotted airfoil

inferred← citeshttps://doi.org/10.1016/j.oceaneng.2020.108209openalex-snapshot

A bio-inspired twin-protuberance hydrofoil design

inferred← citeshttps://doi.org/10.1016/j.oceaneng.2022.111727openalex-snapshot

Flow characteristics and performance of the propulsion system with wavy duct

inferred← citeshttps://doi.org/10.1016/j.oceaneng.2023.116482openalex-snapshot

Effect of aero-shaped vortex generators on NACA 4415 airfoil

inferred← citeshttps://doi.org/10.1016/j.rineng.2026.111629openalex-snapshot

Preliminary study of the effects of leading-edge serration on a two-section planar wing in ground-effect at low Reynolds number

inferred← citeshttps://doi.org/10.1061/jaeeez.aseng-5243openalex-snapshot

Improvement of Poststall Performance of NACA 0015 Airfoil Using Leading-Edge Synthetic Jet Array

inferred← citeshttps://doi.org/10.1063/1.4984677openalex-snapshot

Design modification of airfoil by integrating sinusoidal leading edge and dimpled surface

inferred← citeshttps://doi.org/10.1063/1.5110481openalex-snapshot

Effects of non-uniform permeability on vortex shedding and noise control of blunt trailing edge

inferred← citeshttps://doi.org/10.1063/5.0098400openalex-snapshot

Modeling of the compartmentalization effect induced by leading-edge tubercles

inferred← citeshttps://doi.org/10.1063/5.0120124openalex-snapshot

Airfoil trailing-edge noise and drag reduction at a moderate Reynolds number using wavy geometries

inferred← citeshttps://doi.org/10.1063/5.0156362openalex-snapshot

Investigation of aerodynamic performance of Clark-Y airfoil with more realistic tubercle model and internal slots

inferred← citeshttps://doi.org/10.1063/5.0193391openalex-snapshot

Numerical study on aerodynamic and noise performance of bionic asymmetric airfoil with surface grooves

inferred← citeshttps://doi.org/10.1063/5.0297947openalex-snapshot

Aerodynamic noise reduction of small unmanned aerial vehicle rotors via steady suction and blowing control

inferred← citeshttps://doi.org/10.1063/5.0331580openalex-snapshot

Flow reorganization of a spanwise non-uniform airfoil by a biomorphic wavy leading edge

inferred← citeshttps://doi.org/10.1063/5.0334100openalex-snapshot

Co-flow jet control for separation-induced noise reduction of an airfoil at high angles of attack

inferred← citeshttps://doi.org/10.1063/5.0342673openalex-snapshot

Flow control physics of bio-inspired leading-edge tubercles: Mechanisms, scaling effects, and engineering implications

inferred← citeshttps://doi.org/10.1080/15435075.2022.2050376openalex-snapshot

Flow control of a wind-turbine airfoil with a leading-edge spherical dimple

inferred← citeshttps://doi.org/10.1080/19942060.2016.1277165openalex-snapshot

Numerical simulation of flow characteristics behind the aerodynamic performances on an airfoil with leading edge protuberances

inferred← citeshttps://doi.org/10.1080/19942060.2022.2119282openalex-snapshot

Numerical simulation and dynamic mode decomposition analysis of the flow past wings with spanwise waviness

inferred← citeshttps://doi.org/10.1088/1757-899x/1067/1/012102openalex-snapshot

Investigating the effects of fin geometry on motorcycle cylinder cooling

inferred← citeshttps://doi.org/10.1088/1757-899x/671/1/012144openalex-snapshot

Numerical Study of the Boundary Layer Separation Control on the NACA 0012 Airfoil using Triangular Rib

inferred← citeshttps://doi.org/10.1103/physrevfluids.4.053901openalex-snapshot

Second-order sensitivity in the cylinder wake: Optimal spanwise-periodic wall actuation and wall deformation

inferred← citeshttps://doi.org/10.1103/physrevfluids.5.083901openalex-snapshot

Optimal spanwise-periodic control for recirculation length in a backward-facing step flow

inferred← citeshttps://doi.org/10.1177/0954406220950353openalex-snapshot

Optimization of wavy cylinder for aerodynamic drag and aeroacoustic sound reduction using computational fluid dynamics analysis

inferred← citeshttps://doi.org/10.1177/09544062231185495openalex-snapshot

Investigation of aerodynamic and aeroacoustic behavior of bio-inspired airfoils with numerical and experimental methods

inferred← citeshttps://doi.org/10.1177/0954410016682271openalex-snapshot

The importance of controlling the upstream body wake in tandem cylinders system for noise reduction

inferred← citeshttps://doi.org/10.1177/0954410018812617openalex-snapshot

Numerical investigation of aerodynamic and acoustic characteristics of bionic airfoils inspired by bird wing

inferred← citeshttps://doi.org/10.21203/rs.3.rs-19449/v1openalex-snapshot

Ferrofluid Thin Films for Airfoil Lift Generation

inferred← citeshttps://doi.org/10.2514/1.j056152openalex-snapshot

Experimental Investigation of a Bioinspired Bluff-Body Effect on Galloping Piezoelectric Energy-Harvester Performance

inferred← citeshttps://doi.org/10.2514/1.j060180openalex-snapshot

Influence of Leading-Edge Tubercle with Amplitude Modulation on NACA 0015 Airfoil

inferred← citeshttps://doi.org/10.2514/6.2015-1257openalex-snapshot

Galloping Piezoelectric Energy Harvester with Bio-inspired Square Bluff Body

inferred← citeshttps://doi.org/10.2514/6.2018-3389openalex-snapshot

Crossflow Stability of a Swept Flat Plate with Wavy Leading Edge

inferred← citeshttps://doi.org/10.2514/6.2019-2621openalex-snapshot

Effects of non-uniform permeability on vortex shedding and noise control of blunt trailing edge

inferred← citeshttps://doi.org/10.31436/iiumej.v19i1.784openalex-snapshot

A PARAMETRIC STUDY ON CONTROL OF FLOW SEPARATION OVER AN AIRFOIL IN INCOMPRESSIBLE REGIME

inferred← citeshttps://doi.org/10.3390/app11209634openalex-snapshot

Performance Improvement in a Wavy Twisted Rudder by Alignment of the Wave Peak

inferred← citeshttps://doi.org/10.3390/app12010416openalex-snapshot

Analysis of Influence of Different Parameters on Numerical Simulation of NACA0012 Incompressible External Flow Field under High Reynolds Numbers

inferred← citeshttps://doi.org/10.3390/app13106061openalex-snapshot

Experiment on Noise Reduction of a Wavy Cylinder with a Large Spanwise Wavelength and Large Aspect Ratio in Aeroacoustic Wind Tunnels

inferred← citeshttps://doi.org/10.3934/mina.2024015openalex-snapshot

A two- to three-dimensional wake transition mechanism induced by the angle of attack of a NACA0012 airfoil

inferred← citeshttps://doi.org/10.47176/jafm.15.04.1026openalex-snapshot

Influence of a Wavy Blade-End Applied in an Axial Compressor Cascade on the Secondary Flow of the Passage

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.