NASA NTRS · 19790046589
Shock structure in transonic compressor rotors
Abstract
The inadequacy of axisymmetric theory in modeling the structure of the shock system in a transonic compressor rotor is shown with a simple model. A more accurate model for the flow near the sonic radius is proposed, which is supported by some flow visualization data and three-dimensional computations.
Keep this discovery
Explore connections, maps & timelines
Epstein, A. H., Kerrebrock, J. L., Thompkins, W. T., Jr.. 1979-04-01. Shock structure in transonic compressor rotors. https://ntrs.nasa.gov/citations/19790046589
Cite the original work for its findings. Save a collection to share your selection of sources.