NASA Technical Reports Server (NTRS) 19820008174: Calculation of three-dimensional, inviscid, supersonic, steady flowsReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820008174: Calculation of three-dimensional, inviscid, supersonic, steady flows


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A detailed description of a computational program for the evaluation of three dimensional supersonic, inviscid, steady flow past airplanes is presented. Emphasis was put on how a powerful, automatic mapping technique is coupled to the fluid mechanical analysis. Each of the three constituents of the analysis (body geometry, mapping technique, and ga

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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