Open ErwinMoerland opened 3 years ago
n1rel: relative rotational speed of the low pressure spool = rotational speed based on design speed n1 (maximum take-off) n2rel: relative rotational speed of high pressure spool = rotational speed based on design speed n2 (maximum take-off)
Suggested is to add the following parameters to the engine performanceMap entries (vectors), located at
/cpacs/vehicles/engines/engine/analysis/performanceMaps/performanceMap
:relDryThrust
(relative dry thrust = share of maximum dry thrust, values > 1 mean: using afterburnerrelWetThrust
(relative wet thrust = thrustRatio based on maximum wet thrust, values always < 1)n1rel
(definition to be added)n2rel
(definition to be added)