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Edge geometry of turbomachine blades
- Source :
- NASA Tech Briefs. 3(2)
- Publication Year :
- 1978
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1978.
-
Abstract
- Computer program calculates leading- and trailing-edge circle radii, tangency angles on leading- and trailing-edge circles, and stagger angle of turbomachinery blade sections, using only spline points defining blade surfaces.
- Subjects :
- Mechanics
Subjects
Details
- Language :
- English
- ISSN :
- 0145319X
- Volume :
- 3
- Issue :
- 2
- Database :
- NASA Technical Reports
- Journal :
- NASA Tech Briefs
- Publication Type :
- Report
- Accession number :
- edsnas.19780000262
- Document Type :
- Report