NASA NTRS · 19870013335
Simulation of multistage turbine flows
Abstract
A flow model has been developed for analyzing multistage turbomachinery flows. This model, referred to as the average passage flow model, describes the time-averaged flow field with a typical passage of a blade row embedded within a multistage configuration. Computer resource requirements, supporting empirical modeling, formulation code development, and multitasking and storage are discussed. Illustrations from simulations of the space shuttle main engine (SSME) fuel turbine performed to date are given.
Keep this discovery
Explore connections, maps & timelines
Adamczyk, John J., Mulac, Richard A.. 1987-01-01. Simulation of multistage turbine flows. https://ntrs.nasa.gov/citations/19870013335
Cite the original work for its findings. Save a collection to share your selection of sources.