An 8-Foot Axisymmetrical Fixed Nozzle for Subsonic Mach Numbers Up to 0.99 and for a Supersonic Mach Number of 1.2
Description: From Introduction: "This paper, which should be of interest to those concerned with transonic wind tunnels, covers the design and operating characteristics of the nozzle."
Date: February 23, 1950
Creator: Ritchie, Virgil S.; Wright, Ray H. & Tulin, Marshall P.
Partner: UNT Libraries Government Documents Department