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    Unknown
    In:  Other Sources
    Publication Date: 2019-06-28
    Description: Computer program calculates subsonic or transonic flow on hubshroud, midchannel, stream surface of single-blade row of turbomachine. Program uses finite-different and quasi-orthogonal (velocity-gradient) methods. Program is reported in two volumes: Part I is User's Manual, Part II is Programmer's Manual.
    Keywords: MECHANICS
    Type: LEW-12966 , NASA Tech Briefs (ISSN 0145-319X); 3; 1; P. 100
    Format: text
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