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.
Flow velocities and streamlines
NASA Tech Briefs ; 3 , 1
01.06.1978
Sonstige
Keine Angabe
Englisch
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