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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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BibTeXRIS

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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