NASA NTRS · 19920043102
Three-dimensional simulation of a translating strut inlet
Abstract
A three-dimensional Navier-Stokes code is used to numerically simulate the flow through a translating strut scramjet inlet. The inlet has variable geometry for efficient operation over a wide speed range. Overall flow-field features such as the corner flow, topwall separation, shockwave coalescence, cowl pressure increase, and flow distortion at the throat are investigated. Comparisons are made with experimental results to provide for the assessment of the present analysis. Effects of boundary-layer ingestion on the overall flow features are also investigated.
Keep this discovery
Explore connections, maps & timelines
Singh, D. J., Trexler, Carl A., Hudgens, Julie A.. 1992-01-01. Three-dimensional simulation of a translating strut inlet. https://ntrs.nasa.gov/citations/19920043102
Cite the original work for its findings. Save a collection to share your selection of sources.