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  • [[Category:Pages needing cleanup after Import]] ...
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  • As flight speed builds up after take-off, the ram rise in the intake starts to have a significant effect up [[Category:Pages moved from Wikipedia]] ...
    15 KB (2,389 words) - 03:36, 29 April 2017
  • ...in an estimate of the compressor mass flow, pressure ratio and efficiency. After the combustion calculation is completed, the implied compressor mechanical ...turbine power '''<math>{\delta}P_w\, </math>''', allowed to float instead. After the iteration has converged, the excess power is used to estimate the chang ...
    20 KB (3,137 words) - 17:45, 24 August 2020
  • ...absorbed by these two "components" is taken as the load on the LP turbine. After the Fan Outer compression calculation, there is a Bypass Duct pressure loss [[Category:Pages moved from Wikipedia]] ...
    26 KB (4,131 words) - 17:46, 24 August 2020
  • ...absorbed by these two "components" is taken as the load on the LP turbine. After the Fan Outer compression calculation, there is a Bypass Duct pressure loss ...in an estimate of the compressor mass flow, pressure ratio and efficiency. After the combustion calculation is completed, the implied compressor mechanical ...
    53 KB (8,391 words) - 17:54, 24 August 2020
  • {{Cleanup|<br>This resource needs organization and [[Wikipedia:Chunking|chunking]] th ...ation into the overall design and marketing strategy than to mend mistakes after launch. Political sensitivities include border delimitations and historical ...
    214 KB (31,170 words) - 15:56, 6 February 2024