A parametric differentiation version with finite-difference scheme applicable to a class of problems in boundary layer flow with massive blowing

DOI10.1016/0045-7930(82)90017-2zbMath0477.76039OpenAlexW2094304307MaRDI QIDQ1160533

S. Singh

Publication date: 1982

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(82)90017-2

zbMATH Keywords

finite-difference schemeparametric differentiationmassive blowing

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Basic methods in fluid mechanics (76M99)

Related Items (1)

Unsteady three-dimensional boundary layer flow due to a stretching surface

Cites Work

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• Boundary-layer flow at a saddle point of attachment
• Three-dimensional laminar compressible boundary layers with large injection
• Fast and stable numerical method for boundary-layer flow with massive blowing
• Laminar flow at a three-dimensional stagnation point with large rates of injection
• The equation of similar profiles in boundary layer theory with strong blowing
• Boundary-layer flows with large injection and heat transfer.
• Heat and mass transfer at a general three- dimensional stagnation point.
• Solution of the transonic airfoil problem through parametric differentiation.
• Solution of Nonlinear Flow Problems through Parametric Differentiation
• On laminar boundary-layer blow-off. Part 2
• Shooting Method for Solution of Boundary-Layer Flows with Massive Blowing
• BOUNDARY-LAYER FLOW AT A THREE-DIMENSIONAL STAGNATION POINT WITH STRONG BLOWING

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