NASA Technical Reports Server (NTRS) 19740003001: Analysis and design of three dimensional supersonic nozzles. Volume 2: Numerical program for analysis of nozzle-exhaust flow fieldsReportar como inadecuado




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The FORTRAN IV Program developed to analyze the flow field associated with scramjet exhaust systems is presented. The instructions for preparing input and interpreting output are described. The program analyzes steady three dimensional supersonic flow by the reference plane characteristic technique. The governing equations and numerical techniques

Autor: NASA Technical Reports Server (NTRS)

Fuente: https://archive.org/







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