An approximate analysis for the turbulent boundary layer thickness on a cone in supersonic flow
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Publication:5725444
DOI10.1007/BF03184628zbMath0116.19401OpenAlexW95302121MaRDI QIDQ5725444
Publication date: 1963
Published in: Applied Scientific Research (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf03184628
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