Analysis of Limitations Imposed on One-Spool Turbojet-Engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers
Description: Limitations on turbojet engine design by turbines with downstream stators.
Date: January 19, 1955
Creator: Cavicchi, R. H. & Constantine, A. B.
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Partner: UNT Libraries Government Documents Department