NASA NTRS · 19850021935
Application of computational fluid dynamics to complex inlet ducts
Abstract
A three-dimensional parabolic Navier-Stokes code, PEPSIG, was used to analyze the flow in the subsonic diffuser section of a typical modern inlet design. The effect of curvature of the diffuser centerline and transitioning cross sections was studied to determine the primary cause of flow distortion in the duct. Total pressure values at the engine compressor face are reported.
Keep this discovery
Explore connections, maps & timelines
Towne, C. E., Schum, E. F.. 1985-01-01. Application of computational fluid dynamics to complex inlet ducts. https://ntrs.nasa.gov/citations/19850021935
Cite the original work for its findings. Save a collection to share your selection of sources.