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by IQAC KIITKIIT Deemed to be University — Internal Quality Assurance Cell

Publication2021

Optimal Design of Hysteretic Nonlinear Energy Sink for Suppression of Limit Cycle Oscillations of a Flapping Airfoil

The record

Type
Publication
Date
1 January 2021
Level
International — held abroad
Journal
Lecture Notes in Civil Engineering
Volume
75
Pages
363-375
Published
1 January 2021
DOI
10.1007/978-981-15-4577-1_30
Scopus ID
85088252688
ISSN
23662557
Authors
2
Open access
No
Citations
0
International co-authorship
Yes
Co-author countries
CA, IN

Classification

Every label below carries the reasoning it was assigned on, the confidence band it was assigned in, and what produced it. The rubric is published.

UN Sustainable Development Goals

  1. 9.5 Enhance scientific research, upgrade technological capabilities, and increase researchers and R&D spending

    TargetPrimaryHigh confidenceJudged

    Develops hysteretic nonlinear energy sink with negative stiffness for suppressing aircraft wing oscillations through passive control optimization advancing aerodynamic technology.

    High confidence
    The subject matter is a strong and direct inference from the record type, the funding or organising body, or the programme context, even where the title alone is thin. Example: an ICMR-funded project against SDG 3, on the strength of the agency.
    Judged
    Judged against the published classification rubric, under the rubric and prompt versions recorded with the run that produced it.
    Produced by
    claude-haiku-4-5-20251001, under kortex-publication-v1

  2. 17.6 Enhance North-South, South-South and triangular cooperation on science, technology and innovation, and knowledge sharing

    TargetSecondaryHigh confidenceRule-derivedrule sdg17-structural-v1

    Structural signal: co-authorship outside India.

    Rule-derived
    Emitted by a deterministic rule from structural signals rather than judged from the record’s text. The rule carries a version, so rule-derived and judged labels stay separable.
    Produced by
    sdg17-structural-v1, under kortex-publication-v1

Viksit Bharat @2047

  1. vb-3.1 Research and development

    Sub-themePrimaryHigh confidenceJudged

    Contributes to research and development through advanced vibration control methodology applicable to aerospace and mechanical systems.

    Produced by
    claude-haiku-4-5-20251001, under kortex-publication-v1

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KIIT Deemed to be University. “Optimal Design of Hysteretic Nonlinear Energy Sink for Suppression of Limit Cycle Oscillations of a Flapping Airfoil”. Kortex.

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