NASA NTRS · 19690020682
Characteristic design study of mixed- compression two-dimensional inlets with low-angle cowls for the Mach number range 2.70 to 1.80
Abstract
Design effects on performance of two dimensional mixed-compression supersonic inlets with low angle cowls
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Anderson, B. H.. 1969-07-01. Characteristic design study of mixed- compression two-dimensional inlets with low-angle cowls for the Mach number range 2.70 to 1.80. https://ntrs.nasa.gov/citations/19690020682
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