Some internal-flow characteristics of several axisymmetrical NACA 1-series nose air inlets at zero flight speed
Description:
Report presenting testing of six 1-series axisymmetrical nose air inlets of 8-inch maximum diameter at zero forward velocity in the 8-foot transonic tunnel. Total-pressure surveys, pressure-recovery measurements, and flow-visualization studies were made through a range of mass-flow ratio from below the normal operating range to choking. Results indicate that the performance characteristics of the inlets with differing amounts of roundness varied widely.
Date:
July 15, 1954
Creator:
Bryan, Carroll R. & Fleming, Frank F.
Item Type:
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Partner:
UNT Libraries Government Documents Department