NASA NTRS ยท 19810019516
Some aspects of calculating flows about three-dimensional subsonic inlets
Abstract
Based on the potential flow model, computations were carried out for various three-dimensional inlet models. Some of these calculated results are presented in the forms of surface static pressure, flow angularity, surface flow pattern, and inlet flow field. Comparisons with experimental data are also made.
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Kao, H. C.. 1981-01-01. Some aspects of calculating flows about three-dimensional subsonic inlets. https://ntrs.nasa.gov/citations/19810019516
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