NASA NTRS · 19730000245
A computer program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzles
Abstract
Program uses component performance maps to enable user to do analytical engine cycle calculations. Either convergent or convergent-divergent nozzles may be used.
Keep this discovery
Explore connections, maps & timelines
Fishbach, L. H., Koenig, R. W.. 1973-11-01. A computer program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzles. https://ntrs.nasa.gov/citations/19730000245
Cite the original work for its findings. Save a collection to share your selection of sources.