Shock-free transonic airfoils with a given pressure distribution

DOI10.1016/0045-7825(86)90151-9zbMath0604.76047OpenAlexW2000139018MaRDI QIDQ1083310

B. George

Publication date: 1986

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(86)90151-9

zbMATH Keywords

stream functionairfoil shapepressure distributionfast Poisson solversonic linecharacteristic marching procedurehodograph techniquesinverse design procedureshock-free supercritical airfoilssubcritical portion of the flowsupercritical portion of the flowsupercritical pressure distribution

Mathematics Subject Classification ID

Transonic flows (76H05) Basic methods in fluid mechanics (76M99)

Cites Work

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• Supercritical wing sections. III
• Subsonic airfoils with a given pressure distribution
• Algorithm 541: Efficient Fortran Subprograms for the Solution of Separable Elliptic Partial Differential Equations [D3]
• Iterative solution of transonic flows over airfoils and wings, including flows at mach 1
• Perturbation of a Discontinuous Transonic Flow
• Plane subcritical flow past a lifting aerofoil
• Analysis of transonic airfoils
• Calculation of plane steady transonic flows
• ON THE HODOGRAPH TRANSFORMATION FOR HIGH-SPEED FLOW: II. A FLOW WITH CIRCULATION

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