User's guide for NASCRIN - a vectorized code for calculating two-dimensional supersonic internal flow fields
By: Ajay Kumar.
Contributors: Langley Research Center
Publisher: Langley Research Center
Published: 1984
Place of publication: Hampton, Va
Number of pages: 67
Subjects: Euler equations of motion; Inlet flow; Navier-Stokes equation; Supersonic combustion ramjet engines
Notes: Bibliographical references: p.63.