Second-order small-disturbance solution for wing at supersonic speeds

DOI10.2514/3.13439zbMath0909.76040OpenAlexW2008010968MaRDI QIDQ3839649

Hsien Kei Cheng, Shijun Luo

Publication date: 12 April 1999

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.13439

zbMATH Keywords

integral equationshock wavessecond-order boundary conditionstwo-dimensional airfoilslinearized velocity potential equation

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

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