NASA Technical Reports Server (NTRS) 19840021091: Numerical solution for the interaction of shock wave with laminar boundary layer in two-dimensional flow on a flat plate. Ph.D. ThesisReport as inadecuate



 NASA Technical Reports Server (NTRS) 19840021091: Numerical solution for the interaction of shock wave with laminar boundary layer in two-dimensional flow on a flat plate. Ph.D. Thesis


NASA Technical Reports Server (NTRS) 19840021091: Numerical solution for the interaction of shock wave with laminar boundary layer in two-dimensional flow on a flat plate. Ph.D. Thesis - Download this document for free, or read online. Document in PDF available to download.

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The finite difference computation method was investigated for solving problems of interaction between a shock wave and a laminar boundary layer, through solution of the complete Navier-Stokes equations. This method provided excellent solutions, was simple to perform and needed a relatively short solution time. A large number of runs for various flo

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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