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searching for Overall pressure ratio 8 found (331 total)

alternate case: overall pressure ratio

Jet engine performance (16,813 words) [view diff] exact match in snippet view article find links to article

with overall pressure ratio of about 35:1 which is generated by 1 fan, 4 low pressure and 10 high pressure compressor stages. By 2016 overall pressure ratio
Bristol Janus (509 words) [view diff] exact match in snippet view article find links to article
be so small that an axial unit would be challenging. Sufficient overall pressure ratio was obtained by mounting two centrifugal compressors in series on
IAE V2500 (1,167 words) [view diff] exact match in snippet view article find links to article
Two extra booster stages were required to restore the original overall pressure ratio. A fourth booster stage would be added after the initial variant
GTRE GTX-35VS Kaveri (4,916 words) [view diff] exact match in snippet view article find links to article
GTRE's design envisions achieving a fan pressure ratio of 4:1 and an overall pressure ratio of 27:1, which it believes will permit the Tejas to "supercruise"
Podded engine (1,061 words) [view diff] exact match in snippet view article find links to article
pressure across the fan face acceptable. Pressure losses, and hence overall pressure ratio, affect engine performance or fuel consumption for each pound of
Compressible flow (3,791 words) [view diff] exact match in snippet view article find links to article
through a duct with a minimum area, or sonic throat. Additionally, an overall pressure ratio, Pb/Pt, of approximately 2 is needed to attain Mach 1. Once it has
British Aerospace HOTOL (2,971 words) [view diff] no match in snippet view article find links to article
two heat exchangers to pre-cool the air prior to entering a high overall pressure-ratio turbojet-like engine cycle — the heated hydrogen driving a turbine
Compressor map (6,224 words) [view diff] exact match in snippet view article find links to article
between the fan and the high pressure (HP) compressor to increase overall pressure ratio. US civil engines tend to mount the IP compressor on the LP shaft