Large Lightweight Turbojet Engines

Name: Large Lightweight Turbojet Engines
Creator: C. A. Grinyer

descriptionPublicationkeyboard_double_arrow_right Article , Other literature type 01 Jan 1958Publisher:SAE InternationalJournal:SAE Technical Paper Series, volume 1 (issn: 0148-7191, eissn: 2688-3627,

Authors: C. A. Grinyer;

doi: 10.4271/580033

Large Lightweight Turbojet Engines

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Abstract

<div class="section abstract"><div class="htmlview paragraph">THIS paper deals with the general performance of turbojet engines in both subsonic and supersonic flight in relation to aircraft requirements.</div><div class="htmlview paragraph">The advantages and disadvantages of the bypass engine and small turbojet in relation to the large straight jet engine of 18,000-lb thrust are examined. Also discussed is the improvement in the thrust-weight ratio of large engines made possible by the use of titanium, and the potentialities of ejector nozzles and turbine-blade cooling.</div></div>

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