A scheme for computing near-axisymmetric gas flow and supersonic flow past a cylinder end-face at a low angle of attack
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Publication:3777611
DOI10.1016/0041-5553(86)90137-0zbMath0637.76055OpenAlexW2084004669MaRDI QIDQ3777611
Publication date: 1986
Published in: USSR Computational Mathematics and Mathematical Physics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0041-5553(86)90137-0
trigonometric interpolationboundary conditioncircular cylinder end-face at a low angle of attackcoarse particle methodnear-axisymmetric gas flows
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