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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