Analysis of Off-Design Operation of High Mach Number Supersonic Turbojet Engines
Description:
From Introduction: "Because of the lack of data on compressor characteristics at 130 or 145 percent of design equivalent rotational speed, several simplifying assumptions were made regarding the compressor characteristics during operation at equivalent rotational speeds above the design value (hereinafter called "compressor overspeeding"). In addition to results based on these assumptions, the effect of deviation from these assumptions is discussed."
Date:
February 4, 1954
Creator:
English, Robert E. & Cavicchi, Richard H.
Item Type:
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Partner:
UNT Libraries Government Documents Department