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Calculating Turbine-Blade Loads
- Source :
- NASA Tech Briefs. 12(4)
- Publication Year :
- 1988
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1988.
-
Abstract
- Rotor/stator interactions analyzed with help of approximations. Analytical procedure assists designers of turbomachinery in calculating dynamic loads on blades and vanes. Procedure involves approximations simplifying calculation of phase angles and amplitudes of pressure fields throughout blade and vane rows at each disturbance frequency.
- Subjects :
- Machinery
Subjects
Details
- Language :
- English
- ISSN :
- 0145319X
- Volume :
- 12
- Issue :
- 4
- Database :
- NASA Technical Reports
- Journal :
- NASA Tech Briefs
- Publication Type :
- Report
- Accession number :
- edsnas.19880000256
- Document Type :
- Report