Talk:Shenyang WS-15

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Aviation: Engines

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inlet diameter and thrust

The inlet diameter, projected speed and thrust values do not look credible. The inlet area would be -12% of the comparable P&W F135. A dry thrust of 90kN to 115kN sounds more likely, with some "sources" giving 105kN. I get that there is no information available about an engine that does not exist, just saying that it does not add up. --Moritzgedig (talk) 08:36, 17 July 2020 (UTC)[reply]