NASA NTRS · 19760007039
NNEP: The Navy NASA Engine Program
Abstract
A computer code capable of simulating almost any conceivable turbine engine is described. This code uses stacked component maps and multiple flowpaths to simulate variable cycle engines with variable component geometry. It is capable of design and off-design (matching) calculations and can optimize free variables such as nozzle areas to minimize specific fuel consumption.
Keep this discovery
Explore connections, maps & timelines
Fishbach, L. H., Caddy, M. J.. 1975-12-01. NNEP: The Navy NASA Engine Program. https://ntrs.nasa.gov/citations/19760007039
Cite the original work for its findings. Save a collection to share your selection of sources.