Improvement in aerodynamic performance of NACA0021 airfoil using moving surface boundary layer: A computational study

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ID: 41695
2019
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salam2019improvementaip Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors Salam, M.
Journal AIP Conference Proceedings
Year 2019
DOI 10.1063/1.5115903
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