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NASA NTRS · 20220008149

Exit Boundary Layer Data for Three Rectangular Nozzles at High Subsonic Mach Numbers

Abstract

Exit boundary layer characteristics were measured for three rectangular nozzles to aid numerical simulations. These results are summarized in this presentation.

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BibTeXRIS

Khairul Zaman. Exit Boundary Layer Data for Three Rectangular Nozzles at High Subsonic Mach Numbers. https://ntrs.nasa.gov/citations/20220008149

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