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Average-passage flow model development
- Source :
- Structural Integrity and Durability of Reusable Space Propulsion Systems.
- Publication Year :
- 1989
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1989.
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Abstract
- A 3-D model was developed for simulating multistage turbomachinery flows using supercomputers. This average passage flow model described the time averaged flow field within a typical passage of a bladed wheel within a multistage configuration. To date, a number of inviscid simulations were executed to assess the resolution capabilities of the model. Recently, the viscous terms associated with the average passage model were incorporated into the inviscid computer code along with an algebraic turbulence model. A simulation of a stage-and-one-half, low speed turbine was executed. The results of this simulation, including a comparison with experimental data, is discussed.
- Subjects :
- Fluid Mechanics And Heat Transfer
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Journal :
- Structural Integrity and Durability of Reusable Space Propulsion Systems
- Publication Type :
- Report
- Accession number :
- edsnas.19910015025
- Document Type :
- Report