NASA NTRS · 19800008768
A supersonic three-dimensional code for flow over blunt bodies: Program documentation and test cases
Abstract
The use of a computer code for the calculation of steady, supersonic, three dimensional, inviscid flow over blunt bodies is illustrated. Input and output are given and explained for two cases: a pointed code of 20 deg half angle at 15 deg angle of attack in a free stream with M sub infinite = 7, and a cone-ogive-cylinder at 10 deg angle of attack with M sub infinite = 2.86. A source listing of the computer code is provided.
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Chaussee, D. S., Mcmillan, O. J.. 1980-02-01. A supersonic three-dimensional code for flow over blunt bodies: Program documentation and test cases. https://ntrs.nasa.gov/citations/19800008768
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