NASA NTRS · 19860053742
Analysis of fully stalled compressor
Abstract
An analysis yields a model for energy transfer in compressor stages operating in the closed-throttle condition. The derivation indicates that three geometry parameters (hub/tip ratio, aspect ratio, and rotor blade setting angle) influence the values of pressure coefficient when the compressor flow is close to zero.
Keep this discovery
Explore connections, maps & timelines
Rostafinski, W.. 1986-05-01. Analysis of fully stalled compressor. https://ntrs.nasa.gov/citations/19860053742
Cite the original work for its findings. Save a collection to share your selection of sources.