NASA NTRS · 19780000553
Potential flows in propulsion system inlets
Abstract
Collection of computer programs used to calculate compressible potential flow in arbitrary axisymmetric inlet at any combination of operating conditions of inlet mass-flow rate, free stream velocity, and incident angle proves useful in development of wide variety of propulsion system inlet designs.
Keep this discovery
Explore connections, maps & timelines
Farrell, C. A., Jr., Stockman, N. O.. 1979-03-01. Potential flows in propulsion system inlets. https://ntrs.nasa.gov/citations/19780000553
Cite the original work for its findings. Save a collection to share your selection of sources.