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Search: Posts Made By: latetonite
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Forum: Tech Log
24th Dec 2011, 15:40
Replies: 9
Views: 6,051
Posted By latetonite

V=A x (T exhaust-T inlet), i.e the more temp....

V=A x (T exhaust-T inlet), i.e the more temp. difference you can create, (with a lower OAT and same TIT or EGT) the more thrust you can make. So optimum engine operating altitude should be in theory...
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