NASA NTRS · 19800006790
A supersonic, three-dimensional code for flow over blunt bodies: User's manual
Abstract
A computer code is described which may be used to calculate the steady, supersonic, three-dimensional, inviscid flow over blunt bodies. The theoretical and numerical formulation of the problem is given (shock-capturing, downstream marching), including exposition of the boundary and initial conditions. The overall flow logic of the program, its usage, accuracy, and limitations are discussed.
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Chaussee, D. S., Mcmillan, O. J.. 1980-01-01. A supersonic, three-dimensional code for flow over blunt bodies: User's manual. https://ntrs.nasa.gov/citations/19800006790
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