An Investigation of the Drag of Windshields in the 8-Foot High-Speed Wind Tunnel
Description:
"The drag of closed-cockpit and transport-type windshields was determined from tests made at speeds from 200 to 440 miles per hour in the NACA 8-foot high-speed wind tunnel. This speed range corresponds to a test Reynolds number range of 2,510,000 to 4,830,000 based on the mean aerodynamic chord of the full-span model (17.29 inches). The shapes of the windshield proper, the hood, and the tail fairing were systematically varied to include common types and a refined design" (p. 1).
Date:
June 1939
Creator:
Robinson, Russell G. & Delano, James B.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department