Evidence map›Paper›PMID 41857067›Full record

ArticleScientific reports2026

CFD-driven neural network and SVM models for airfoil aerodynamic enhancement with bio-inspired riblets and plasma actuation.

Kailam Vijayakumar Karthikeyan, Amritha Raju, Jake Jain, Srinivasan Lekshmanan, Harish Rajan

Abstract read
In one paragraph

Article in Scientific reports, 2026. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Not yet cited in PubMed.

0numbers the graph read from it
0cells of the map it votes in
0citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

0 citing papers in PubMed.

No citing paper in PubMed yet.

4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

5 authors.

Kailam Vijayakumar KarthikeyanSchool of Mechanical Engineering, Vellore Institute of Technology, Chennai, Tamil Nadu, 600127, India.
Amritha RajuSchool of Mechanical Engineering, Vellore Institute of Technology, Chennai, Tamil Nadu, 600127, India.
Jake JainSchool of Mechanical Engineering, Vellore Institute of Technology, Chennai, Tamil Nadu, 600127, India.
Srinivasan LekshmananSchool of Mechanical Engineering, Vellore Institute of Technology, Chennai, Tamil Nadu, 600127, India.
Harish RajanSchool of Mechanical Engineering, Vellore Institute of Technology, Chennai, Tamil Nadu, 600127, India. harish.r@vit.ac.in.

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

Enhancing the airfoil performance using advanced flow control techniques is an important challenge in the aerospace and automotive industries. In this article a hybrid computational and artificial intelligence (AI) approach is developed for aerodynamic performance enhancement of a NACA4412 airfoil by using a combination of bio inspired riblets and active plasma control. Semi circular, triangular and fillet riblets were tested with alternating current dielectric barrier discharge (AC-DBD) plasma devices and simulations were performed using computational fluid dynamics (CFD) technique at a Reynolds number of [Formula: see text] with angles of attack ranging from [Formula: see text] to [Formula: see text]. The performance assessment parameters considered in this work include lift coefficient [Formula: see text], drag coefficient [Formula: see text], lift to drag ratio ([Formula: see text]) ratio and vorticity contours in order to infer flow stability and efficiency. The simulation results indicated a reduced drag coefficient using riblets due to modifications in wall boundary layers along with a subsequent addition of AC-DBD devices to suppress vortex formation, delay separation and promote higher lift. Among all designs the bio-inspired fillet riblet with plasma actuator recorded maximum improvements with respect to [Formula: see text] with an increase of [Formula: see text] and [Formula: see text] in [Formula: see text] ratio with respect to base configuration. Additionally, to facilitate model prediction and simulation the machine learning algorithms were established using artificial neural networks with scaled conjugate gradient learning algorithm and support vector machine regressions. The results obtained indicated excellent model accuracy with high correlation coefficient and low mean squared error measurements using [Formula: see text] and [Formula: see text] predictions. These findings highlight the dual role of CFD and AI in the optimization of flow control strategies and confirm that the integration of physics based simulations with machine learning offers an efficient and reliable pathway for prediction and design innovation in aerodynamics.

Indexed as

Aerodynamic performanceArtificial neural networkBio-inspired ribletsCFD-machine learning integrationScaled conjugate gradientSupport vector machine

Identifiers

PMID41857067
PMCPMC13139372

What OpenQuestion holds

Textmetadata
LicenceCC BY
Read underepoch 390

Registered trials

None linked

Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.