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

Clicks: 154
ID: 41695
2019
Reference Key
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
URL
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